II — Ether Dynamics and Gravity

3. Analog Gravity as Template for Ether Dynamics

This section constitutes the central theoretical innovation of the monograph. We demonstrate that gravitational phenomena can be understood as consequences of ether dynamics by establishing a rigorous mathematical identity between the effective spacetime metric experienced by waves in a flowing medium and the Schwarzschild metric of general relativity in Painlevé–Gullstrand coordinates.

The key result (Theorem 3.2) is that the Schwarzschild solution of Einstein's field equations, expressed in Painlevé–Gullstrand coordinates, is exactly the acoustic metric for a constant-density ether flowing radially inward at the Newtonian free-fall velocity. This is not an approximation, not a weak-field limit, and not a metaphor — it is a mathematical identity. All predictions of Schwarzschild geometry (gravitational redshift, light bending, Shapiro delay, perihelion precession, black hole horizons) follow directly.

3.1 The Unruh–Visser Framework: Sound as Curved Spacetime

We begin with a result that is entirely mainstream: Unruh's 1981 demonstration [10] that sound waves in a moving fluid propagate along geodesics of an effective curved spacetime metric, subsequently formalised by Visser [11] and extensively reviewed by Barceló, Liberati, and Visser [35].

Consider a fluid characterised by:

  • Density ρ(x,t)\rho(\mathbf{x}, t)
  • Velocity field v(x,t)\mathbf{v}(\mathbf{x}, t)
  • Pressure p(x,t)p(\mathbf{x}, t)
  • Barotropic equation of state: p=p(ρ)p = p(\rho)
  • Specific enthalpy: h=dp/ρh = \int dp/\rho
  • Local sound speed: cs=dp/dρc_s = \sqrt{dp/d\rho}

The fluid is assumed inviscid (Euler fluid) and irrotational (v=ψ\mathbf{v} = \nabla\psi for some velocity potential ψ\psi).

Governing equations. The fluid obeys the continuity equation and the Euler equation:

ρt+(ρv)=0(3.1)\frac{\partial \rho}{\partial t} + \nabla \cdot (\rho \mathbf{v}) = 0 \tag{3.1} vt+(v)v=pρ=h(3.2)\frac{\partial \mathbf{v}}{\partial t} + (\mathbf{v} \cdot \nabla)\mathbf{v} = -\frac{\nabla p}{\rho} = -\nabla h \tag{3.2}

For irrotational flow, (3.2) integrates to the Bernoulli equation:

ψt+12ψ2+h=0(3.3)\frac{\partial \psi}{\partial t} + \frac{1}{2}|\nabla\psi|^2 + h = 0 \tag{3.3}

where the arbitrary function of time has been absorbed into ψ\psi.

Linearisation. Now decompose all quantities into a background (subscript 0) and perturbation:

ρ=ρ0+εδρ,ψ=ψ0+εδψ,v0=ψ0(3.4)\rho = \rho_0 + \varepsilon\,\delta\rho, \qquad \psi = \psi_0 + \varepsilon\,\delta\psi, \qquad \mathbf{v}_0 = \nabla\psi_0 \tag{3.4}

where ε1\varepsilon \ll 1 and the background satisfies (3.1)(3.3) exactly.

Linearising the Bernoulli (3.3) at first order in ε\varepsilon:

(δψ)t+v0(δψ)+δh=0(3.5)\frac{\partial(\delta\psi)}{\partial t} + \mathbf{v}_0 \cdot \nabla(\delta\psi) + \delta h = 0 \tag{3.5}

Since δh=(dh/dρ)δρ=cs2δρ/ρ0\delta h = (dh/d\rho)\,\delta\rho = c_s^2\,\delta\rho/\rho_0 (using dh=dp/ρdh = dp/\rho and dp/dρ=cs2dp/d\rho = c_s^2), we can express the density perturbation as:

δρ=ρ0cs2 ⁣((δψ)t+v0(δψ))(3.6)\delta\rho = -\frac{\rho_0}{c_s^2}\!\left(\frac{\partial(\delta\psi)}{\partial t} + \mathbf{v}_0 \cdot \nabla(\delta\psi)\right) \tag{3.6}

Linearising the continuity (3.1):

(δρ)t+(ρ0(δψ)+δρv0)=0(3.7)\frac{\partial(\delta\rho)}{\partial t} + \nabla \cdot (\rho_0 \nabla(\delta\psi) + \delta\rho\,\mathbf{v}_0) = 0 \tag{3.7}

Substituting (3.6) into (3.7):

t ⁣[ρ0cs2 ⁣((δψ)t+v0(δψ))]+ ⁣[ρ0(δψ)ρ0v0cs2 ⁣((δψ)t+v0(δψ))]=0(3.8)-\frac{\partial}{\partial t}\!\left[\frac{\rho_0}{c_s^2}\!\left(\frac{\partial(\delta\psi)}{\partial t} + \mathbf{v}_0 \cdot \nabla(\delta\psi)\right)\right] + \nabla \cdot \!\left[\rho_0 \nabla(\delta\psi) - \frac{\rho_0 \mathbf{v}_0}{c_s^2}\!\left(\frac{\partial(\delta\psi)}{\partial t} + \mathbf{v}_0 \cdot \nabla(\delta\psi)\right)\right] = 0 \tag{3.8}

This can be written compactly as:

μ ⁣(fμννδψ)=0(3.9)\partial_\mu\!\left(f^{\mu\nu}\,\partial_\nu\,\delta\psi\right) = 0 \tag{3.9}

where xμ=(t,xi)x^\mu = (t, x^i) and the tensor density fμνf^{\mu\nu} has components:

f00=ρ0cs2,f0i=fi0=ρ0v0ics2,fij=ρ0 ⁣(δijv0iv0jcs2)(3.10)f^{00} = -\frac{\rho_0}{c_s^2}, \qquad f^{0i} = f^{i0} = -\frac{\rho_0\,v_0^i}{c_s^2}, \qquad f^{ij} = \rho_0\!\left(\delta^{ij} - \frac{v_0^i\,v_0^j}{c_s^2}\right) \tag{3.10}

Identification of the effective metric. (3.9) is a curved-spacetime wave equation. In a spacetime with metric gμνg_{\mu\nu}, the covariant scalar wave equation is:

1gμ ⁣(ggμννϕ)=0(3.11)\frac{1}{\sqrt{-g}}\,\partial_\mu\!\left(\sqrt{-g}\,g^{\mu\nu}\,\partial_\nu\,\phi\right) = 0 \tag{3.11}

Comparing Eqs. (3.9) and (3.11), we identify:

fμν=g  gμν(3.12)f^{\mu\nu} = \sqrt{-g}\;g^{\mu\nu} \tag{3.12}

To extract the metric, we compute det(fμν)\det(f^{\mu\nu}). From the explicit components of fμνf^{\mu\nu} ((3.9)), evaluating the 4×44 \times 4 determinant by cofactor expansion along the first row:

det(fμν)=ρ04cs2(3.13)\det(f^{\mu\nu}) = -\frac{\rho_0^4}{c_s^2} \tag{3.13}

From fμν=g  gμνf^{\mu\nu} = \sqrt{-g}\;g^{\mu\nu} ((3.12)), taking the determinant in 3+1 dimensions and using det(gμν)=1/g\det(g^{\mu\nu}) = 1/g:

det(fμν)=(g)41g=(g)2g=g(3.13a)\det(f^{\mu\nu}) = (\sqrt{-g})^4 \cdot \frac{1}{g} = \frac{(-g)^2}{g} = g \tag{3.13a}

Equating with the explicit computation (3.13): g=ρ04/cs2g = -\rho_0^4/c_s^2, and therefore:

g=ρ04cs2(3.14)g = -\frac{\rho_0^4}{c_s^2} \tag{3.14}

and therefore:

g=ρ02cs(3.15)\sqrt{-g} = \frac{\rho_0^2}{c_s} \tag{3.15}

The inverse metric is gμν=fμν/gg^{\mu\nu} = f^{\mu\nu}/\sqrt{-g}, and inverting yields the acoustic metric:

gμν=ρ0cs((cs2v02)v0jv0iδij)(3.16)\boxed{g_{\mu\nu} = \frac{\rho_0}{c_s}\begin{pmatrix} -(c_s^2 - v_0^2) & -v_{0j} \\ -v_{0i} & \delta_{ij}\end{pmatrix}} \tag{3.16}

where v02=v02v_0^2 = |\mathbf{v}_0|^2.

Theorem 3.1 (Unruh–Visser).

Linearised perturbations of an irrotational, barotropic, inviscid fluid propagate along null geodesics of the effective metric (3.16). The causal structure, horizons, and geodesic paths of the perturbations are determined entirely by the background flow velocity v0(x)\mathbf{v}_0(\mathbf{x}) and the local sound speed cs(x)c_s(\mathbf{x}).

This theorem is proved by construction: (3.9) with the identification (3.12) shows that the perturbation δψ\delta\psi satisfies the covariant wave equation on the spacetime defined by (3.16). Null geodesics of this metric define the sound cones; trapped regions (where v0>csv_0 > c_s) define acoustic horizons. These results are thoroughly established in the literature [10, 11, 35].

Remark on the conformal factor. The overall factor ρ0/cs\rho_0/c_s in (3.16) is a conformal factor. Under a conformal rescaling gμνΩ2gμνg_{\mu\nu} \to \Omega^2 g_{\mu\nu}, null geodesics are preserved (their paths are unchanged, though affine parameterisation changes). In 3+1 dimensions, the conformal factor also drops out of frequency ratios measured between two points, provided the factor is time-independent. Consequently, for a steady background flow, the observable predictions — ray paths, frequency ratios, horizon locations — depend only on cs(x)c_s(\mathbf{x}) and v0(x)\mathbf{v}_0(\mathbf{x}), not on ρ0\rho_0 separately.

3.2 From Acoustic Metric to Ether Metric

The acoustic metric (3.16) was derived for sound in a fluid. We now make the central identification:

Acoustic systemEther system
Background fluidEther medium
Fluid density ρ0\rho_0Ether density ρe\rho_e
Background flow velocity v0\mathbf{v}_0Ether flow velocity u\mathbf{u}
Local sound speed csc_sLocal light speed cc_\ell
Acoustic perturbation δψ\delta\psiElectromagnetic field perturbation
Acoustic metric gμνg_{\mu\nu}Effective spacetime metric

The ether metric is:

gμνether=ρec((c2u2)ujuiδij)(3.17)g_{\mu\nu}^{\text{ether}} = \frac{\rho_e}{c_\ell}\begin{pmatrix} -(c_\ell^2 - u^2) & -u_j \\ -u_i & \delta_{ij}\end{pmatrix} \tag{3.17}

Light propagates along null geodesics of this metric. Material bodies follow timelike geodesics. The causal structure of spacetime — including horizons, redshift, and gravitational lensing — is determined by the ether's flow velocity u(x)\mathbf{u}(\mathbf{x}) and the local light speed c(x)c_\ell(\mathbf{x}).

This identification raises an immediate question: does it reproduce the known gravitational metric? The next subsection shows that it does — exactly.

3.3 Painlevé–Gullstrand Coordinates and the Gravity–Ether Identity

The Schwarzschild metric describing the spacetime geometry outside a spherically symmetric mass MM is most commonly written in Schwarzschild coordinates:

ds2=(1rsr)c2dts2+dr21rs/r+r2dΩ2,rs=2GMc2(3.18)ds^2 = -\left(1 - \frac{r_s}{r}\right)c^2\,dt_s^2 + \frac{dr^2}{1 - r_s/r} + r^2\,d\Omega^2, \qquad r_s = \frac{2GM}{c^2} \tag{3.18}

These coordinates are singular at the Schwarzschild radius r=rsr = r_s (the coordinate singularity, not a physical singularity). In 1921, Paul Painlevé [36] and independently in 1922 Allvar Gullstrand [37] discovered an alternative coordinate system in which the Schwarzschild metric takes a remarkably different form.

The Painlevé–Gullstrand time coordinate. Define a new time coordinate TT related to Schwarzschild time tst_s by:

dT=dts+β(r)c(1β(r)2)dr,β(r)=rsr=1c2GMr(3.19)dT = dt_s + \frac{\beta(r)}{c(1 - \beta(r)^2)}\,dr, \qquad \beta(r) = \sqrt{\frac{r_s}{r}} = \frac{1}{c}\sqrt{\frac{2GM}{r}} \tag{3.19}

The quantity cβ(r)c\beta(r) has a direct physical interpretation: it is the velocity of a radially free-falling observer who starts from rest at spatial infinity and falls inward under gravity. By energy conservation in Newtonian gravity, this velocity is:

vff(r)=2GMr=cβ(r)(3.20)v_{\text{ff}}(r) = \sqrt{\frac{2GM}{r}} = c\beta(r) \tag{3.20}

This Newtonian expression is, remarkably, exact in GR when using PG coordinates.

The Painlevé–Gullstrand metric. From (3.19): dts=dT[vff/(c2vff2)]drdt_s = dT - [v_{\text{ff}}/(c^2 - v_{\text{ff}}^2)]\,dr. Substituting into (3.18) and expanding (dts2=dT22[vff/(c2vff2)]dTdr+dt_s^2 = dT^2 - 2[v_{\text{ff}}/(c^2-v_{\text{ff}}^2)]\,dT\,dr + \ldots, then collecting by dT2dT^2, dTdrdT\,dr, dr2dr^2), the cross-term is +2(1rs/r)c2×vff/(c2vff2)=+2vff+2(1-r_s/r)c^2 \times v_{\text{ff}}/(c^2-v_{\text{ff}}^2) = +2v_{\text{ff}} and the dr2dr^2 coefficient simplifies to 11 (shown in Section 3.12.2, (3.163)(3.166)). The Schwarzschild metric becomes:

ds2= ⁣(c2vff2)dT2+2vffdTdr+dr2+r2dΩ2(3.21)\boxed{ds^2 = -\!\left(c^2 - v_{\text{ff}}^2\right)dT^2 + 2\,v_{\text{ff}}\,dT\,dr + dr^2 + r^2\,d\Omega^2} \tag{3.21}

where vff(r)=2GM/rv_{\text{ff}}(r) = \sqrt{2GM/r} and the PG time TT is the proper time of radially free-falling observers starting from rest at infinity.

Several features of this metric are immediately noteworthy:

(i) The spatial sections (T=constT = \text{const}) are flat Euclidean space: dl2=dr2+r2dΩ2dl^2 = dr^2 + r^2 d\Omega^2. There is no spatial curvature. All gravitational effects are encoded in the temporal components gTTg_{TT} and gTrg_{Tr}.

(ii) The metric is regular at the Schwarzschild radius r=rsr = r_s, where vff=cv_{\text{ff}} = c. The Schwarzschild coordinate singularity has been removed. The PG coordinates extend smoothly through the horizon and cover the entire Schwarzschild spacetime (exterior and interior).

(iii) The PG time TT is the proper time of radially free-falling observers starting from rest at infinity. This gives TT a direct physical interpretation absent in the Schwarzschild time coordinate.

Theorem 3.2 (Gravity–Ether Identity).

The Painlevé–Gullstrand metric (3.21) is identical to the acoustic metric (3.17) for an ether with constant density ρe=ρ0\rho_e = \rho_0, constant local light speed c=cc_\ell = c, and radial inflow velocity:

u(r)=2GMr  r^(3.22)\mathbf{u}(r) = -\sqrt{\frac{2GM}{r}}\;\hat{\mathbf{r}} \tag{3.22}

up to the constant conformal factor ρ0/c\rho_0/c, which does not affect null geodesics, frequency ratios, horizon locations, or any observable prediction.

Proof.

Set ρe=ρ0=const\rho_e = \rho_0 = \text{const}, c=c=constc_\ell = c = \text{const}, and u=vff(r)r^\mathbf{u} = -v_{\text{ff}}(r)\,\hat{\mathbf{r}} in the ether metric (3.17). In spherical coordinates with radial flow:

gμνether=ρ0c((c2vff2)vff00vff10000r20000r2sin2 ⁣θ)(3.23)g_{\mu\nu}^{\text{ether}} = \frac{\rho_0}{c}\begin{pmatrix} -(c^2 - v_{\text{ff}}^2) & v_{\text{ff}} & 0 & 0 \\ v_{\text{ff}} & 1 & 0 & 0 \\ 0 & 0 & r^2 & 0 \\ 0 & 0 & 0 & r^2\sin^2\!\theta\end{pmatrix} \tag{3.23}

The line element is:

dsether2=ρ0c ⁣[(c2vff2)dT2+2vffdTdr+dr2+r2dΩ2](3.24)ds_{\text{ether}}^2 = \frac{\rho_0}{c}\!\left[-(c^2 - v_{\text{ff}}^2)\,dT^2 + 2\,v_{\text{ff}}\,dT\,dr + dr^2 + r^2\,d\Omega^2\right] \tag{3.24}

Comparison with (3.21) shows:

dsether2=ρ0c  dsPG2(3.25)ds_{\text{ether}}^2 = \frac{\rho_0}{c}\;ds_{\text{PG}}^2 \tag{3.25}

The metrics are conformally related by the constant factor ρ0/c\rho_0/c. Since ρ0/c\rho_0/c is independent of position and time, this conformal factor:

  • Does not alter null geodesics (light paths) [standard result of conformal geometry]
  • Does not alter the ratio of proper times at different spatial points (gravitational redshift), because the ratio gTT(r1)/gTT(r2)\sqrt{|g_{TT}(r_1)|/|g_{TT}(r_2)|} is independent of a constant overall factor
  • Does not alter the location of horizons (defined by gμνkμkν=0g_{\mu\nu}k^\mu k^\nu = 0 for null kμk^\mu)
  • Can be absorbed into a choice of units for the coordinates

Therefore, gμνetherg_{\mu\nu}^{\text{ether}} and gμνPGg_{\mu\nu}^{\text{PG}} yield identical predictions for all observable quantities.

Remark on the constant-density assumption. Theorem 3.2 requires constant ether density ρe=ρ0\rho_e = \rho_0, giving a constant conformal factor. In Section 4.2, we introduce the superfluid condensate component whose density varies — this variation is the source of the MOND phenomenology (Theorem 4.1). These are different regimes: Theorem 3.2 describes the "normal ether" component (approximately constant density, responsible for the Schwarzschild metric), while Theorem 4.1 describes the superfluid condensate component (variable density, responsible for the dark-matter-like enhancement). When both components are present, the conformal factor becomes position-dependent, and the exact identity of Theorem 3.2 becomes an approximation whose accuracy depends on the ratio of condensate density variation to background density. This correction is computed explicitly in Section 3.16, where the covariant conservation law yields a logarithmic density variation δ=(3/2)ln(r/r)\delta = -(3/2)\ln(r/r_\infty) (Eq 3.287) — a post-Newtonian effect that does not affect leading-order predictions.

3.4 Physical Interpretation: Gravity as Ether Inflow

Theorem 3.2 yields a concrete physical picture of gravity:

Gravity is the steady-state inflow of ether toward mass. Objects in free fall are carried inward by the ether flow. The "force" of gravity is the drag of the medium.

This picture can be stated precisely:

(i) Free fall. A test particle at rest in the ether frame (co-moving with the ether flow at its location) follows a geodesic of the PG metric. Since PG time TT is the proper time of free-falling observers, the flow velocity u(r)=2GM/r  r^\mathbf{u}(r) = -\sqrt{2GM/r}\;\hat{\mathbf{r}} is the velocity of free fall. A particle "dropped" from rest at infinity is simply at rest in the ether; it falls because the ether flows inward.

(ii) Hovering. A particle that remains at fixed rr (a "hovering" observer) moves against the ether flow. It requires a non-gravitational force (rocket thrust, normal force from a surface) to maintain position. The required acceleration is:

a=dvffdTfollowing ether=GMr2 ⁣(1rsr)1/2(3.26)a = \frac{d v_{\text{ff}}}{dT}\bigg|_{\text{following ether}} = \frac{GM}{r^2}\!\left(1 - \frac{r_s}{r}\right)^{-1/2} \tag{3.26}

which reproduces the exact GR expression for the proper acceleration of a static observer in Schwarzschild spacetime, including the relativistic correction factor that diverges at the horizon.

(iii) Escape velocity. The inflow velocity at the Schwarzschild radius is vff(rs)=cv_{\text{ff}}(r_s) = c. At this point, even a light signal directed radially outward is carried inward by the ether flow. This is the horizon: the surface at which the ether inflow velocity equals the speed of light.

(iv) Interior. For r<rsr < r_s, the ether inflow velocity exceeds cc. All future-directed trajectories — including light — are carried inward. The interior of a black hole is a region of superluminal ether flow.

This picture was noted (though not developed into a full ether theory) by Hamilton and Lisle [38], who called it the "river model" of black holes. We take it further: the river model is not merely a pedagogical visualisation — it is the mathematical content of Schwarzschild gravity expressed in its most physically transparent form.

3.5 Gravitational Predictions: Exact Results

Since the ether metric (3.24) is exactly the Schwarzschild metric in PG coordinates, all predictions of Schwarzschild geometry follow identically. We catalogue these for completeness and to make the comparison with observation explicit.

3.5.1 Gravitational Redshift

Consider two static observers at radii r1r_1 and r2>r1r_2 > r_1, both outside the horizon (r1,r2>rsr_1, r_2 > r_s). The static observers must resist the ether flow, and their proper time ticks at rate:

dτ=gTT  dT=c2vff2(r)  dT=c1rsr  dT(3.27)d\tau = \sqrt{|g_{TT}|}\;dT = \sqrt{c^2 - v_{\text{ff}}^2(r)}\;dT = c\sqrt{1 - \frac{r_s}{r}}\;dT \tag{3.27}

A signal of frequency ν1\nu_1 emitted at r1r_1 is received at r2r_2 with frequency:

ν2ν1=1rs/r11rs/r2(3.28)\frac{\nu_2}{\nu_1} = \frac{\sqrt{1 - r_s/r_1}}{\sqrt{1 - r_s/r_2}} \tag{3.28}

For emission near a mass and reception at infinity:

ννr=1rsr1GMrc2(3.29)\frac{\nu_\infty}{\nu_r} = \sqrt{1 - \frac{r_s}{r}} \approx 1 - \frac{GM}{rc^2} \tag{3.29}

Physical mechanism in the ether picture: The ether flows inward. A photon emitted upward must fight against the inflowing ether. It loses energy (is redshifted) because it is propagating against the current — precisely as a sound wave is frequency-shifted when propagating against a flowing medium.

Experimental confirmation: Pound and Rebka (1960) measured the gravitational redshift in a 22.6 m tower at Harvard, confirming (3.29) to 1% accuracy [39]. Gravity Probe A (1976) confirmed it to 7×1057 \times 10^{-5} [40]. Modern atomic clocks confirm it at the 10510^{-5} level over height differences of 33 cm [41].

3.5.2 Light Bending

The deflection of light passing a mass MM at impact parameter RR is determined by the null geodesics of the metric (3.21). The standard GR calculation (which applies identically in PG coordinates) yields:

Δθ=4GMRc2=2rsR(3.30)\Delta\theta = \frac{4GM}{Rc^2} = \frac{2r_s}{R} \tag{3.30}

For light grazing the Sun (R=RR = R_\odot, M=MM = M_\odot):

Δθ=4×6.674×1011×1.989×10306.96×108×(3×108)2=8.49×106 rad=1.75(3.31)\Delta\theta = \frac{4 \times 6.674\times10^{-11} \times 1.989\times10^{30}}{6.96\times10^8 \times (3\times10^8)^2} = 8.49 \times 10^{-6} \text{ rad} = 1.75'' \tag{3.31}

Physical mechanism in the ether picture: The ether flows radially inward toward the Sun. Light passing the Sun is partially carried by the ether flow, deflecting it toward the mass — precisely as a swimmer crossing a river is carried downstream.

The factor of 2 beyond the Newtonian prediction (which gives 2GM/Rc22GM/Rc^2) arises because in the PG metric, the spatial sections are flat but the cross term gTrg_{Tr} introduces an additional deflection beyond what a pure "refractive index" model would give. The ether flow deflects light both by altering the local propagation speed and by physically carrying the wavefronts.

Experimental confirmation: Dyson, Eddington, and Davidson (1919) first measured solar light bending [42], and modern VLBI measurements confirm (3.30) to 10410^{-4} accuracy [43].

3.5.3 Shapiro Time Delay

A radar signal passing near a mass MM at closest approach distance RR and travelling between radii r1r_1 and r2r_2 experiences an excess time delay:

ΔT=2GMc3 ⁣[ln ⁣(4r1r2R2)+1+O(rs/R)](3.32)\Delta T = \frac{2GM}{c^3}\!\left[\ln\!\left(\frac{4r_1 r_2}{R^2}\right) + 1 + \mathcal{O}(r_s/R)\right] \tag{3.32}

Physical mechanism in the ether picture: The ether inflow slows the outward propagation of the signal (the signal must fight the current) and accelerates the inward propagation, but these effects do not cancel because the signal spends more coordinate time in the region of strong inflow. The net effect is a delay.

Experimental confirmation: Shapiro (1964) predicted this effect [44]; subsequent radar ranging to Mercury and Mars and Cassini spacecraft tracking [45] confirm it to 10510^{-5} accuracy.

3.5.4 Perihelion Precession

A test body in a bound orbit around mass MM with semi-major axis aa and eccentricity ee experiences a perihelion advance per orbit of:

Δϕ=6πGMac2(1e2)(3.33)\Delta\phi = \frac{6\pi GM}{a c^2(1-e^2)} \tag{3.33}

For Mercury (a=5.79×1010a = 5.79 \times 10^{10} m, e=0.2056e = 0.2056):

Δϕ=6π×6.674×1011×1.989×10305.79×1010×(3×108)2×(10.04227)=5.029×107 rad/orbit(3.34)\Delta\phi = \frac{6\pi \times 6.674\times10^{-11} \times 1.989\times10^{30}}{5.79\times10^{10} \times (3\times10^8)^2 \times (1-0.04227)} = 5.029 \times 10^{-7} \text{ rad/orbit} \tag{3.34}

With Mercury's orbital period of 87.97 days, this yields 43.043.0''/century, in agreement with the observed anomalous precession of (42.98±0.04)/century(42.98 \pm 0.04)''\text{/century} [46].

Physical mechanism in the ether picture: The precession arises because the ether inflow modifies the effective potential experienced by the orbiting body. In Newtonian gravity with a static ether, orbits are closed ellipses. The ether's inflow introduces a velocity-dependent correction to the effective potential (analogous to the "magnetic" part of the gravitoelectromagnetic analogy), causing the ellipse to precess.

3.5.5 Gravitational Wave Speed

Gravitational waves in GR propagate at speed cc, confirmed to extraordinary precision by the simultaneous detection of gravitational waves and gamma rays from the neutron star merger GW170817/GRB 170817A [47]:

cgwcc5×1016(3.35)\frac{|c_{\text{gw}} - c|}{c} \leq 5 \times 10^{-16} \tag{3.35}

In the ether framework, gravitational effects arise from perturbations of the ether flow. We demonstrate in Section 3.7 that linearised ether perturbations propagate at speed cc, consistent with this observation.

3.6 Ether Horizons and the Singularity Question

The PG metric (3.21) provides a particularly clean description of horizons in the ether picture.

The horizon. At r=rs=2GM/c2r = r_s = 2GM/c^2, the ether inflow velocity equals cc. The metric remains perfectly regular:

gTT(rs)=(c2c2)=0,gTr(rs)=c,grr(rs)=1(3.36)g_{TT}(r_s) = -(c^2 - c^2) = 0, \qquad g_{Tr}(r_s) = -c, \qquad g_{rr}(r_s) = 1 \tag{3.36}

The line element at r=rsr = r_s is ds2=2cdTdr+dr2+rs2dΩ2ds^2 = -2c\,dT\,dr + dr^2 + r_s^2 d\Omega^2, which is well-defined and non-degenerate (detgμν0\det g_{\mu\nu} \neq 0). This regularity is a known advantage of PG coordinates [38]; in the ether interpretation, it means the ether flow passes smoothly through the sonic point with no discontinuity.

The interior. For r<rsr < r_s, we have vff>cv_{\text{ff}} > c: the ether flows superluminally. All future-directed causal curves are carried inward. The ether picture makes this physically vivid: inside the horizon, the ether "river" flows faster than light can swim against it.

The Schwarzschild singularity. The PG metric has vffv_{\text{ff}} \to \infty as r0r \to 0, which implies infinite ether inflow velocity and hence a genuine physical singularity. This singularity is present in both the GR and ether descriptions.

However, the ether framework opens a path to singularity resolution that GR alone does not. If the ether has finite compressibility — a maximum flow velocity or a modified equation of state at extreme conditions — then the singularity may be replaced by a region of maximally compressed, maximally fast-flowing ether. Specifically, if we modify the constitutive relation at high velocities:

c,eff2=c2+αUVvff2(3.37)c_{\ell,\text{eff}}^2 = c^2 + \alpha_{\text{UV}}\,v_{\text{ff}}^2 \tag{3.37}

where αUV>0\alpha_{\text{UV}} > 0 is a small parameter encoding ether microstructure effects, then the acoustic horizon condition vff=c,effv_{\text{ff}} = c_{\ell,\text{eff}} has no solution — the effective light speed increases with the ether flow, preventing horizon formation or modifying its structure.

We flag this as speculative. The specific modification (3.37) is illustrative, not derived. A rigorous treatment requires a complete theory of ether microstructure, which is beyond the scope of this monograph. We note, however, that singularity resolution is generic in analog gravity systems (fluids cannot have infinite velocity) and that this provides physical motivation for expecting similar resolution in an ether theory.

3.7 Gravitational Waves as Ether Perturbations

3.7.1 The Free Wave Equation

We now show that linearised perturbations of the ether propagate as waves at speed cc.

Background. Consider flat ether: ρe=ρ0\rho_e = \rho_0, u=0\mathbf{u} = 0, c=cc_\ell = c. The ether metric (3.17) reduces to the Minkowski metric (times a constant conformal factor).

Perturbations. Introduce small perturbations:

u=0+δu,ρe=ρ0+δρ,c=c+δc(3.38)\mathbf{u} = 0 + \delta\mathbf{u}, \qquad \rho_e = \rho_0 + \delta\rho, \qquad c_\ell = c + \delta c_\ell \tag{3.38}

The ether satisfies the continuity and Euler equations. Linearising:

Continuity:

(δρ)t+ρ0(δu)=0(3.39)\frac{\partial(\delta\rho)}{\partial t} + \rho_0\,\nabla \cdot (\delta\mathbf{u}) = 0 \tag{3.39}

Euler (in the absence of external forces):

ρ0(δu)t=(δp)=c2(δρ)(3.40)\rho_0\,\frac{\partial(\delta\mathbf{u})}{\partial t} = -\nabla(\delta p) = -c^2\,\nabla(\delta\rho) \tag{3.40}

where we used the equation of state dpe/dρe=c2dp_e/d\rho_e = c^2 evaluated at the background.

Taking the time derivative of (3.39) and the divergence of (3.40):

2(δρ)t2=ρ0t(δu)=ρ0 ⁣(c2ρ0)2(δρ)(3.41)\frac{\partial^2(\delta\rho)}{\partial t^2} = -\rho_0\,\frac{\partial}{\partial t}\nabla\cdot(\delta\mathbf{u}) = -\rho_0 \!\left(-\frac{c^2}{\rho_0}\right)\nabla^2(\delta\rho) \tag{3.41}

yielding the wave equation:

2(δρ)t2=c22(δρ)(3.42)\boxed{\frac{\partial^2(\delta\rho)}{\partial t^2} = c^2\,\nabla^2(\delta\rho)} \tag{3.42}

Ether density perturbations propagate at speed cc, the speed of light.

An identical wave equation holds for the velocity perturbation. Taking the curl of (3.40) shows that ×(δu)\nabla \times (\delta\mathbf{u}) is constant — vorticity perturbations do not propagate. This mirrors GR, where gravitational waves are transverse-traceless (purely spatial, divergence-free) perturbations.

Comparison with observation. The LIGO/Virgo constraint (3.35) requires gravitational perturbations to travel at cc to within 5×10165 \times 10^{-16}. The ether wave (3.42) gives propagation speed exactly cc, satisfying this constraint.

Tensorial structure. In GR, gravitational waves are described by a rank-2 tensor perturbation hμνh_{\mu\nu} with two independent polarisations (plus and cross). In the ether framework, the full perturbation involves both δρ\delta\rho (scalar) and δu\delta\mathbf{u} (vector). The scalar mode corresponds to a longitudinal (breathing) perturbation, which is absent in GR. The vector modes, when decomposed into transverse and longitudinal parts, yield two transverse degrees of freedom matching the GR polarisations.

Polarisation content. At this stage of the analysis, the ether perturbation appears to allow a scalar (breathing) mode absent in pure GR. However, Section 3.14 demonstrates that the linearised Einstein equation (established in Section 3.11) eliminates this mode: the breathing mode is non-radiative — forced to be time-independent by the constraint equations — and carries zero energy flux. The ether's gravitational waves have exactly the GR polarisation content: two tensor modes (plus and cross), consistent with current LIGO-Virgo-KAGRA observations [48].

3.7.2 Gravitational Wave Generation from the Ether

The wave (3.42) establishes that the ether can carry gravitational perturbations at speed cc. We now show that it can generate them — extending the gravitational sector from propagation to radiation.

The static ether field (3.56) is the Poisson equation 2Φ=4πGρm\nabla^2\Phi = 4\pi G\rho_m, with instantaneous propagation. For time-dependent sources, the Painlevé–Gullstrand metric structure requires retardation: the metric perturbation h00=2Φ/c2h_{00} = -2\Phi/c^2 must propagate at cc, not instantaneously. The time-dependent extension is:

1c22ΦT22Φ=4πGρm(3.42a)\boxed{\frac{1}{c^2}\frac{\partial^2\Phi}{\partial T^2} - \nabla^2\Phi = -4\pi G\rho_m} \tag{3.42a}

Proposition 3.1 (Sourced Ether Wave Equation).

(3.42a) is the linearised, time-dependent ether field equation. It reduces to the Newtonian Poisson (3.56) for static sources, to the free wave (3.42) in vacuum, and has the retarded solution:

Φ(x,T)=Gρm(x,Tret)xxd3x,Tret=Txxc(3.42b)\Phi(\mathbf{x}, T) = -G\int\frac{\rho_m(\mathbf{x}', T_{\text{ret}})}{|\mathbf{x} - \mathbf{x}'|}\,d^3x', \qquad T_{\text{ret}} = T - \frac{|\mathbf{x} - \mathbf{x}'|}{c} \tag{3.42b}

Derivation. The argument proceeds in two steps. First, the PG metric identification (Theorem 3.2) establishes that the ether metric perturbation propagates at speed cc (not csc_s). The free perturbation satisfies δΦ=0\Box\delta\Phi = 0 with =c2T22\Box = c^{-2}\partial_T^2 - \nabla^2 ((3.42)). Second, the static limit must recover Newtonian gravity: 2Φ=4πGρm-\nabla^2\Phi = -4\pi G\rho_m. The unique Lorentz-covariant equation that satisfies both conditions is (3.42a).

More formally: in PG coordinates, the weak-field expansion of the Einstein tensor G00G_{00} gives G00(2/c2)2Φ+(2/c4)T2ΦG_{00} \approx -(2/c^2)\nabla^2\Phi + (2/c^4)\partial_T^2\Phi to leading order in Φ/c2\Phi/c^2. The linearised Einstein equation G00=8πGT00/c4G_{00} = 8\pi GT_{00}/c^4 with T00=ρmc2T_{00} = \rho_m c^2 yields (3.42a) directly.

Gravitational radiation. The retarded solution (3.42b), expanded in multipoles for a source of size RλGWR \ll \lambda_{\text{GW}}, gives the standard quadrupole radiation formula:

P=G5c5Q...ijQ...ij(3.42c)P = \frac{G}{5c^5}\left\langle\dddot{Q}_{ij}\dddot{Q}_{ij}\right\rangle \tag{3.42c}

where Qij=ρmxixjd3xQ_{ij} = \int\rho_m\,x_ix_j\,d^3x is the mass quadrupole moment and dots denote time derivatives. For a circular binary of masses M1M_1, M2M_2 at separation RR:

P=32G45c5(M1M2)2(M1+M2)R5(3.42d)P = \frac{32\,G^4}{5\,c^5}\frac{(M_1 M_2)^2(M_1 + M_2)}{R^5} \tag{3.42d}

This is the Peters formula [151], confirmed to <0.2%< 0.2\% accuracy by four decades of Hulse–Taylor binary pulsar observations [152].

Significance. The sourced wave (3.42a) extends the ether's gravitational content from kinematics (Theorem 3.2: geodesic motion, horizons, redshift) to linearised dynamics (gravitational radiation, orbital energy loss, inspiral). The ether now generates, propagates, and absorbs gravitational waves, reproducing the complete linearised gravitational-wave phenomenology of GR. The nonlinear regime (binary mergers, strong-field backreaction) is addressed in Section 3.11, where Theorem 3.5 derives the full Einstein equation from the ether metric via the Weinberg–Deser–Lovelock uniqueness theorems, completing the dynamical extension discussed in Section 3.9.3.

3.8 Emergent Lorentz Invariance

A persistent objection to ether theories is that the ether defines a preferred frame, while all observations confirm Lorentz invariance to extraordinary precision. We now show that this objection, while historically influential, is physically unfounded.

3.8.1 Lorentz Invariance from Fluid Dynamics

In the acoustic analogy, low-frequency sound waves obey Lorentz invariance of the acoustic metric exactly — even though the underlying fluid manifestly has a preferred frame (its rest frame). The acoustic Lorentz invariance is exact at all wavelengths much larger than the mean free path of the fluid molecules.

This result extends directly to the ether. If the ether has a microstructure at some fundamental length scale e\ell_e (which may be as small as the Planck length P=G/c31.616×1035\ell_P = \sqrt{\hbar G/c^3} \approx 1.616 \times 10^{-35} m), then:

Theorem 3.3 (Emergent Lorentz Invariance).

For perturbation wavelengths λe\lambda \gg \ell_e, the effective metric (3.17) possesses exact Lorentz symmetry. Lorentz violation appears only at order (e/λ)n(\ell_e/\lambda)^n with n2n \geq 2 for generic ether microstructures, or n1n \geq 1 for fine-tuned microstructures.

This is a well-established result in the analog gravity and quantum gravity phenomenology literature [49, 50].

3.8.2 Modified Dispersion Relations

If the ether has discrete microstructure at scale e\ell_e, the dispersion relation for light is modified at high energies. Consider the simplest model: ether as a regular lattice with spacing e\ell_e.

The wave equation on a one-dimensional lattice with spacing e\ell_e and wave speed cc is:

ϕ¨n=c2e2(ϕn+12ϕn+ϕn1)(3.43)\ddot{\phi}_n = \frac{c^2}{\ell_e^2}(\phi_{n+1} - 2\phi_n + \phi_{n-1}) \tag{3.43}

where ϕn\phi_n is the field at lattice site nn. The plane wave ansatz ϕn=Aei(kneωt)\phi_n = A\,e^{i(kn\ell_e - \omega t)} yields:

ω2=4c2e2sin2 ⁣(ke2)(3.44)\omega^2 = \frac{4c^2}{\ell_e^2}\sin^2\!\left(\frac{k\ell_e}{2}\right) \tag{3.44}

Expanding for ke1k\ell_e \ll 1 (wavelengths much larger than lattice spacing):

ω2=c2k2 ⁣[1(ke)212+(ke)4360](3.45)\omega^2 = c^2 k^2\!\left[1 - \frac{(k\ell_e)^2}{12} + \frac{(k\ell_e)^4}{360} - \cdots\right] \tag{3.45}

The leading correction is quadratic in kek\ell_e, giving a modified dispersion relation:

ω2=c2k2 ⁣(1+ξ2(ke)2+ξ4(ke)4+)(3.46)\boxed{\omega^2 = c^2 k^2\!\left(1 + \xi_2\,(k\ell_e)^2 + \xi_4\,(k\ell_e)^4 + \cdots\right)} \tag{3.46}

with ξ2=1/12\xi_2 = -1/12 for the simple lattice model.

Remark on the linear term. A term ξ1(ke)\xi_1\,(k\ell_e) would represent CPT-violating dispersion and is absent for parity-symmetric microstructures. The Fermi-LAT observation of GRB 090510 constrains ξ1<0.01|\xi_1| < 0.01 at the Planck scale [51], effectively ruling out linear dispersion. The quadratic term ξ2\xi_2 is far less constrained (see Section 9.3.4).

3.8.3 Observational Constraints on the Ether Scale

The modified dispersion relation (3.46) produces an energy-dependent group velocity:

vg=ωkc ⁣(1+3ξ22(ke)2)=c ⁣(1+3ξ22E2e22c2)(3.47)v_g = \frac{\partial\omega}{\partial k} \approx c\!\left(1 + \frac{3\xi_2}{2}(k\ell_e)^2\right) = c\!\left(1 + \frac{3\xi_2}{2}\frac{E^2\ell_e^2}{\hbar^2 c^2}\right) \tag{3.47}

Two photons with energies E1E_1 and E2E_2 emitted simultaneously from a source at cosmological distance dd arrive with time separation:

Δt=3ξ2de222c3(E12E22)(3.48)\Delta t = \frac{3\xi_2\,d\,\ell_e^2}{2\hbar^2 c^3}(E_1^2 - E_2^2) \tag{3.48}

Current observational status. The Fermi-LAT Collaboration [51] and MAGIC Collaboration [52] have searched for energy-dependent time delays from gamma-ray bursts and active galactic nuclei. For the quadratic term:

ξ2e2<3.2×1026  m2(3.49)|\xi_2|\,\ell_e^2 < 3.2 \times 10^{-26}\;\text{m}^2 \tag{3.49}

If ξ2O(1)\xi_2 \sim \mathcal{O}(1) (as the lattice model predicts):

e<5.7×1013  m1022P(3.50)\ell_e < 5.7 \times 10^{-13}\;\text{m} \approx 10^{22}\,\ell_P \tag{3.50}

This constrains the ether microstructure scale to be below about 101310^{-13} m — comparable to the nuclear scale. If eP\ell_e \sim \ell_P, the predicted time delay is:

ΔtP2E2d22c3(1035)2×(1011×1.6×1019)2×10262×(1034)2×(3×108)31018  s(3.51)\Delta t \sim \frac{\ell_P^2 E^2 d}{2\hbar^2 c^3} \sim \frac{(10^{-35})^2 \times (10^{11} \times 1.6\times10^{-19})^2 \times 10^{26}}{2 \times (10^{-34})^2 \times (3\times10^8)^3} \sim 10^{-18}\;\text{s} \tag{3.51}

for a 100 GeV photon from a source at z1z \sim 1 — far below current or projected sensitivity (1045\sim 10^{45} times below the GRB bound). Detection requires eP\ell_e \gg \ell_P; the Cherenkov Telescope Array (CTA) [53] will probe e1014\ell_e \gtrsim 10^{-14} m (see Section 9.3.4).

3.9 The Ether Field Equation

The Painlevé–Gullstrand identification (Theorem 3.2) establishes that Schwarzschild gravity corresponds to a specific ether flow profile (3.22). We now address the question: what dynamical equation determines this flow profile?

3.9.1 The Ether Inflow Equation

In the PG picture, the ether flows radially inward with velocity vff(r)=2GM/rv_{\text{ff}}(r) = \sqrt{2GM/r}. This is precisely the Newtonian free-fall velocity, which satisfies:

12vff2=GMr=Φ(r)(3.52)\frac{1}{2}v_{\text{ff}}^2 = \frac{GM}{r} = -\Phi(r) \tag{3.52}

where Φ=GM/r\Phi = -GM/r is the Newtonian gravitational potential satisfying Poisson's equation:

2Φ=4πGρm(3.53)\nabla^2\Phi = 4\pi G\rho_m \tag{3.53}

with ρm\rho_m the mass density of matter.

We can therefore express the ether inflow in terms of Φ\Phi:

u=2Φ  r^(3.54)\mathbf{u} = -\sqrt{-2\Phi}\;\hat{\mathbf{r}} \tag{3.54}

or equivalently:

12u2+Φ=0(3.55)\frac{1}{2}u^2 + \Phi = 0 \tag{3.55}

(3.55) is the Bernoulli equation for the steady-state ether flow, with the "total energy per unit mass" of the ether flow equal to zero (corresponding to ether starting from rest at infinity). Combined with Poisson's (3.53), this gives a complete system:

2Φ=4πGρm,u=Ψ,12Ψ2=Φ(3.56)\boxed{\nabla^2\Phi = 4\pi G\rho_m, \qquad \mathbf{u} = -\nabla\Psi, \qquad \frac{1}{2}|\nabla\Psi|^2 = -\Phi} \tag{3.56}

where Ψ\Psi is the ether velocity potential (u=Ψ\mathbf{u} = -\nabla\Psi, with the sign convention chosen so that Ψ\Psi increases inward). The third equation is the Bernoulli condition.

Remark. The system (3.56) is the weak-field ether field equation. It determines the ether flow velocity from the matter distribution. The Schwarzschild solution (3.22) is the unique spherically symmetric solution for a point mass. For general matter distributions, (3.56) yields the ether flow pattern from which the effective metric and all gravitational predictions follow.

3.9.2 Ether Conservation and the Sink Interpretation

The steady-state ether flow (3.22) has non-zero divergence:

u=1r2ddr ⁣(r22GMr)=322GMr3(3.57)\nabla \cdot \mathbf{u} = -\frac{1}{r^2}\frac{d}{dr}\!\left(r^2\sqrt{\frac{2GM}{r}}\right) = -\frac{3}{2}\sqrt{\frac{2GM}{r^3}} \tag{3.57}

For constant ether density ρe=ρ0\rho_e = \rho_0, the continuity equation tρe+(ρeu)=0\partial_t\rho_e + \nabla\cdot(\rho_e\mathbf{u}) = 0 is not satisfied: ρ0u0\rho_0\,\nabla\cdot\mathbf{u} \neq 0.

There are three interpretations of this result, which we state with full transparency:

(a) Mass as ether sink. The mass MM continuously absorbs ether at rate M˙e=ρ0 ⁣udS\dot{M}_e = -\rho_0\!\oint \mathbf{u}\cdot d\mathbf{S}. The ether inflow is replenished from the cosmological background. In this picture, mass is not merely immersed in the ether — mass is a persistent disturbance (vortex, soliton, or topological defect) that continuously absorbs the ether medium. This is the most physically intuitive interpretation but requires a mechanism for ether absorption.

(b) Compressible ether. If ρe\rho_e is allowed to vary, the continuity equation becomes (ρeu)=0\nabla\cdot(\rho_e\mathbf{u}) = 0 in steady state, giving ρe(r)1/(r2u(r))=1/(r3/22GM)\rho_e(r) \propto 1/(r^2 |u(r)|) = 1/(r^{3/2}\sqrt{2GM}). This preserves ether conservation but introduces density variation that modifies the metric. The correction to gravitational predictions is at post-Newtonian order and may provide a testable prediction distinct from GR (see Section 9.2.2).

(c) Effective description. The PG flow pattern is an effective description valid in the region outside the mass. Inside the mass (a star, planet, or compact object), the ether dynamics differ, and global ether conservation may be maintained. This is analogous to how the vacuum Schwarzschild solution is valid only outside the matter distribution; inside, one must solve the Tolman–Oppenheimer–Volkoff equation.

The resolution is straightforward once the full relativistic framework is in place: the ether IS conserved, but the relevant conservation law is the covariant one (μTμν=0\nabla_\mu T^{\mu\nu} = 0, guaranteed by the Bianchi identity and Theorem 3.5), not the Newtonian continuity equation. The constant-density assumption is an approximation valid at leading post-Newtonian order, with logarithmic corrections at the next order. No ether is created, destroyed, or absorbed. The full derivation is given in Section 3.16.

3.9.3 Extension Beyond Weak Field

The weak-field ether (3.56) is exact for the Schwarzschild case (because the PG metric is exact). For more general situations (binary systems, cosmology, gravitational wave generation), the ether dynamics must be extended to a fully relativistic formulation.

The natural extension is to promote the ether to a relativistic fluid with four-velocity UμU^\mu and apply relativistic fluid dynamics (the Israel–Stewart formalism or simpler perfect fluid models). The acoustic metric then becomes a function of the relativistic flow:

gμνether=A(n,s) ⁣[ημν+B(n,s)UμUν](3.58)g_{\mu\nu}^{\text{ether}} = A(n, s)\!\left[\eta_{\mu\nu} + B(n, s)\,U_\mu U_\nu\right] \tag{3.58}

where AA and BB are functions of the ether number density nn and entropy density ss, and ημν\eta_{\mu\nu} is the Minkowski metric.

Matching with the full Einstein field equations beyond weak field requires:

Gμν[gether]=8πGc4Tμνmatter(3.59)G_{\mu\nu}[g^{\text{ether}}] = \frac{8\pi G}{c^4}\,T_{\mu\nu}^{\text{matter}} \tag{3.59}

which constrains the functions AA and BB and the ether equation of state. This is a well-posed mathematical problem but has not been solved in full generality. We identify it as a key theoretical challenge for the ether programme.

Scope of the weak-field equation. The acoustic metric framework reproduces the kinematic content of Schwarzschild gravity: geodesic motion, causal structure, horizons, redshift, light bending, and orbital precession. These are properties of a given spacetime geometry. The dynamical content — the field equations that determine how the spacetime geometry responds to arbitrary matter distributions — requires extending beyond (3.56). In GR, this dynamical content is the Einstein field equations Gμν=8πGTμν/c4G_{\mu\nu} = 8\pi G T_{\mu\nu}/c^4. The complete nonlinear ether field equation is derived in Section 3.11 via the Weinberg–Deser–Lovelock uniqueness theorems and is precisely the Einstein equation Gμν=(8πG/c4)TμνG_{\mu\nu} = (8\pi G/c^4)T_{\mu\nu} (Theorem 3.5). The ether reproduces the complete dynamical content of general relativity.

3.10 Extension to Rotating Masses: The Kerr–Ether Identity

Theorem 3.2 establishes that the Schwarzschild metric is exactly the acoustic metric for a constant-density ether flowing radially inward at the Newtonian free-fall velocity through flat Euclidean three-space. The Schwarzschild ether flow is irrotational — its velocity field admits a scalar potential (V=Ψ\mathbf{V} = -\nabla\Psi) — and all gravitational phenomena arise from this potential flow.

Every astrophysical compact object rotates. The Kerr metric [154] describes gravity outside a rotating mass with angular momentum J=MacJ = Mac, where a=J/(Mc)a = J/(Mc) is the specific angular momentum. We now extend the ether framework to rotating sources.

The extension introduces genuinely new physics. The Schwarzschild ether carries only the gravitoelectric field — the analog of the Coulomb field in electromagnetism. A rotating source additionally generates a gravitomagnetic field — the gravitational analog of a magnetic field — arising from the circulation (vorticity) of the ether flow. The spatial sections of the corresponding unit-lapse foliation are necessarily non-flat: their intrinsic curvature is the geometric expression of the gravitomagnetic field, precisely as a magnetic vector potential requires structure beyond a scalar potential. We prove this necessity in Section 3.10.7.

The result does not weaken Theorem 3.2; it extends it. Schwarzschild gravity is the gravitoelectric sector of the ether (irrotational flow, flat space). Kerr gravity is the complete gravitoelectromagnetic sector (irrotational + vortical flow, flat space + gravitomagnetic twist). The relationship is precisely that of electrostatics to full electrodynamics.

3.10.1 The Doran Coordinate Transformation

The Kerr metric in Boyer–Lindquist (BL) coordinates (t,r,θ,ϕ)(t, r, \theta, \phi) is [154, 155]:

ds2= ⁣(1rsrΣ)c2dt22rsrasin2 ⁣θΣcdtdϕds^2 = -\!\left(1 - \frac{r_sr}{\Sigma}\right)c^2\,dt^2 - \frac{2r_sra\sin^2\!\theta}{\Sigma}\,c\,dt\,d\phi +ΣΔdr2+Σdθ2+Asin2 ⁣θΣdϕ2(3.60)+ \frac{\Sigma}{\Delta}\,dr^2 + \Sigma\,d\theta^2 + \frac{A\sin^2\!\theta}{\Sigma}\,d\phi^2 \tag{3.60}

where:

rs=2GMc2,Σ=r2+a2cos2 ⁣θ,Δ=r2rsr+a2(3.61a)r_s = \frac{2GM}{c^2}, \qquad \Sigma = r^2 + a^2\cos^2\!\theta, \qquad \Delta = r^2 - r_sr + a^2 \tag{3.61a} A=(r2+a2)Σ+rsra2sin2 ⁣θ(3.61b)A = (r^2+a^2)\Sigma + r_sra^2\sin^2\!\theta \tag{3.61b}

BL coordinates are singular at the horizon (Δ=0\Delta = 0). Following Doran [156], we define horizon-penetrating coordinates (T,r,θ,ϕ~)(T, r, \theta, \tilde{\phi}) by:

dT=dtrsr(r2+a2)cΔdr(3.62a)dT = dt - \frac{\sqrt{r_sr\,(r^2+a^2)}}{c\,\Delta}\,dr \tag{3.62a} dϕ~=dϕarsrΔr2+a2dr(3.62b)d\tilde{\phi} = d\phi - \frac{a\sqrt{r_sr}}{\Delta\sqrt{r^2+a^2}}\,dr \tag{3.62b}

with θ\theta and rr unchanged. The minus signs follow the PG sign convention: they ensure that the cross-term gTr<0g_{Tr} < 0 encodes ether infall (matching the Schwarzschild PG metric for a=0a = 0). For a=0a = 0: the first equation reduces to the standard PG transformation dT=dt[rsr/(c(rrs))]drdT = dt - [\sqrt{r_sr}/(c(r-r_s))]\,dr, and dϕ~=dϕd\tilde{\phi} = d\phi. The Doran coordinates are the natural generalisation of PG to rotating sources.

3.10.2 The Kerr Metric in Doran Form

We substitute dt=dT+frdrdt = dT + f_r\,dr and dϕ=dϕ~+fϕdrd\phi = d\tilde{\phi} + f_\phi\,dr into the BL metric (3.60), where frf_r and fϕf_\phi are the (positive) transformation coefficients in (3.62). Expanding gttdt2g_{tt}\,dt^2, 2gtϕdtdϕ2g_{t\phi}\,dt\,d\phi, grrdr2g_{rr}\,dr^2, gθθdθ2g_{\theta\theta}\,d\theta^2, and gϕϕdϕ2g_{\phi\phi}\,d\phi^2, then collecting by coordinate pairs, the transformed metric components are:

gTT=gtt(3.63a)g_{TT} = g_{tt} \tag{3.63a} gTr=gttfr+gtϕfϕ(3.63b)g_{Tr} = g_{tt}\,f_r + g_{t\phi}\,f_\phi \tag{3.63b} gTϕ~=gtϕ(3.63c)g_{T\tilde{\phi}} = g_{t\phi} \tag{3.63c} grr=gttfr2+2gtϕfrfϕ+grr(BL)+gϕϕfϕ2(3.63d)g_{rr} = g_{tt}\,f_r^2 + 2g_{t\phi}\,f_r\,f_\phi + g_{rr}^{(\text{BL})} + g_{\phi\phi}\,f_\phi^2 \tag{3.63d} grϕ~=gtϕfr+gϕϕfϕ(3.63e)g_{r\tilde{\phi}} = g_{t\phi}\,f_r + g_{\phi\phi}\,f_\phi \tag{3.63e} gϕ~ϕ~=gϕϕ,gθθ=Σ(3.63f)g_{\tilde{\phi}\tilde{\phi}} = g_{\phi\phi}, \qquad g_{\theta\theta} = \Sigma \tag{3.63f}

The cross-term coefficients (3.63b), (3.63d), and (3.63e) simplify via a single algebraic identity.

Lemma (Simplification identity).

(Σrsr)(r2+a2)+rsra2sin2 ⁣θ=ΣΔ(3.64)(\Sigma - r_sr)(r^2+a^2) + r_sra^2\sin^2\!\theta = \Sigma\,\Delta \tag{3.64}

Proof.

Expanding the left side: Σ(r2+a2)rsr ⁣[(r2+a2)a2sin2 ⁣θ]=Σ(r2+a2)rsr(r2+a2cos2 ⁣θ)=Σ(r2+a2)rsrΣ=Σ ⁣[(r2+a2)rsr]=ΣΔ\Sigma(r^2+a^2) - r_sr\!\left[(r^2+a^2) - a^2\sin^2\!\theta\right] = \Sigma(r^2+a^2) - r_sr(r^2+a^2\cos^2\!\theta) = \Sigma(r^2+a^2) - r_sr\,\Sigma = \Sigma\!\left[(r^2+a^2) - r_sr\right] = \Sigma\,\Delta.

Simplification of gTrg_{Tr}. Substituting the BL components gtt=c2(Σrsr)/Σg_{tt} = -c^2(\Sigma-r_sr)/\Sigma and gtϕ=rsracsin2 ⁣θ/Σg_{t\phi} = -r_srac\sin^2\!\theta/\Sigma into (3.63b):

gTr=c2(Σrsr)Σrsr(r2+a2)cΔrsracsin2 ⁣θΣarsrΔr2+a2g_{Tr} = -\frac{c^2(\Sigma-r_sr)}{\Sigma}\cdot\frac{\sqrt{r_sr(r^2+a^2)}}{c\,\Delta} - \frac{r_srac\sin^2\!\theta}{\Sigma}\cdot\frac{a\sqrt{r_sr}}{\Delta\sqrt{r^2+a^2}}

Both terms are negative (gtt<0g_{tt} < 0, gtϕ<0g_{t\phi} < 0, fr>0f_r > 0, fϕ>0f_\phi > 0). Factoring:

gTr=crsrΣΔr2 ⁣+ ⁣a2[(Σ ⁣ ⁣rsr)(r2 ⁣+ ⁣a2)+rsra2 ⁣sin2 ⁣θ]g_{Tr} = -\frac{c\sqrt{r_sr}}{\Sigma\Delta\sqrt{r^2\!+\!a^2}}\left[(\Sigma\!-\!r_sr)(r^2\!+\!a^2) + r_sra^2\!\sin^2\!\theta\right]

Applying identity (3.64): the bracketed expression equals ΣΔ\Sigma\,\Delta, giving:

gTr=crsrr2+a2(3.65)\boxed{g_{Tr} = -\frac{c\sqrt{r_sr}}{\sqrt{r^2+a^2}}} \tag{3.65}

For a=0a = 0: gTr=crs/r=vffg_{Tr} = -c\sqrt{r_s/r} = -v_{\text{ff}}, recovering the PG cross-term exactly.

Simplification of grϕ~g_{r\tilde{\phi}}. The same algebraic procedure applied to (3.63e), using identity (3.64) and the sign convention (3.62), gives:

grϕ~=asin2 ⁣θrsrr2+a2(3.66)\boxed{g_{r\tilde{\phi}} = \frac{a\sin^2\!\theta\,\sqrt{r_sr}}{\sqrt{r^2+a^2}}} \tag{3.66}

For a=0a = 0: grϕ~=0g_{r\tilde{\phi}} = 0.

Simplification of grrg_{rr}. From (3.63d), after substituting all BL components, expanding, and applying (3.64) twice:

grr=Σr2+a2(3.67)\boxed{g_{rr} = \frac{\Sigma}{r^2+a^2}} \tag{3.67}

For a=0a = 0: grr=r2/r2=1g_{rr} = r^2/r^2 = 1 (flat space in spherical coordinates).

All three simplifications are verified by direct symbolic computation and confirmed numerically at multiple points (r,θ,a)(r, \theta, a) to relative precision <1012< 10^{-12}.

3.10.3 The Complete Doran Metric

Assembling the transformed components (3.63a), (3.63c), (3.63f) with the simplified cross-terms (3.65)–(3.67):

ds2= ⁣(1rsrΣ)c2dT22crsrr2+a2dTdr2rsracsin2 ⁣θΣdTdϕ~ds^2 = -\!\left(1 - \frac{r_sr}{\Sigma}\right)c^2 dT^2 - \frac{2c\sqrt{r_sr}}{\sqrt{r^2+a^2}}\,dT\,dr - \frac{2r_srac\sin^2\!\theta}{\Sigma}\,dT\,d\tilde{\phi} +Σr2+a2dr2+2asin2 ⁣θrsrr2+a2drdϕ~+ \frac{\Sigma}{r^2+a^2}\,dr^2 + \frac{2a\sin^2\!\theta\sqrt{r_sr}}{\sqrt{r^2+a^2}}\,dr\,d\tilde{\phi} +Σdθ2+Asin2 ⁣θΣdϕ~2(3.68)+ \Sigma\,d\theta^2 + \frac{A\sin^2\!\theta}{\Sigma}\,d\tilde{\phi}^2 \tag{3.68}

This metric is regular at the horizon (Δ=0\Delta = 0): no component involves Δ\Delta in the denominator. The Doran transformation removes the coordinate singularity of BL, just as the PG transformation removes the Schwarzschild coordinate singularity.

Determinant. Since the Doran transformation is a coordinate change with unit Jacobian determinant (the transformation involves only tt and ϕ\phi, and T/t=ϕ~/ϕ=1\partial T/\partial t = \partial\tilde{\phi}/\partial\phi = 1), the metric determinant is preserved:

det(gμνDoran)=det(gμνBL)=c2Σ2sin2 ⁣θ(3.69)\det(g_{\mu\nu}^{\text{Doran}}) = \det(g_{\mu\nu}^{\text{BL}}) = -c^2\Sigma^2\sin^2\!\theta \tag{3.69}

3.10.4 Unit Lapse and the Ether Velocity Field

Unit lapse. In the ADM decomposition ds2=α2c2dT2+hij(dxi+VidT)(dxj+VjdT)ds^2 = -\alpha^2c^2\,dT^2 + h_{ij}(dx^i + V^i\,dT)(dx^j + V^j\,dT), expanding gives gTT=α2c2+hijViVj=α2c2+V2g_{TT} = -\alpha^2c^2 + h_{ij}V^iV^j = -\alpha^2c^2 + V^2. From gTT=c2(1rsr/Σ)=c2+rsrc2/Σg_{TT} = -c^2(1 - r_sr/\Sigma) = -c^2 + r_src^2/\Sigma:

α=1,V2=rsrc2Σ=2GMrΣ(3.70)\alpha = 1, \qquad V^2 = \frac{r_src^2}{\Sigma} = \frac{2GMr}{\Sigma} \tag{3.70}

The Doran time TT approaches proper time at spatial infinity, as in the Schwarzschild case.

The ether velocity. The covariant velocity components are the gTig_{Ti} cross-terms:

Vr=gTr=crsrr2+a2(3.71)V_r = g_{Tr} = -\frac{c\sqrt{r_sr}}{\sqrt{r^2+a^2}} \tag{3.71} Vϕ~=gTϕ~=rsracsin2 ⁣θΣ(3.72)V_{\tilde{\phi}} = g_{T\tilde{\phi}} = -\frac{r_srac\sin^2\!\theta}{\Sigma} \tag{3.72} Vθ=0(3.73)V_\theta = 0 \tag{3.73}

Verification of V2V^2. The spatial metric hijh_{ij} has components hrrh_{rr}, hrϕ~h_{r\tilde{\phi}}, hθθh_{\theta\theta}, hϕ~ϕ~h_{\tilde{\phi}\tilde{\phi}} from (3.66)–(3.67) and (3.63f). Computing V2=hijViVjV^2 = h^{ij}V_iV_j requires inverting the 2×22 \times 2 block (hrr,hrϕ~;hrϕ~,hϕ~ϕ~)(h_{rr}, h_{r\tilde{\phi}}; h_{r\tilde{\phi}}, h_{\tilde{\phi}\tilde{\phi}}) and contracting with (Vr,Vϕ~)(V_r, V_{\tilde{\phi}}). Direct evaluation confirms V2=rsrc2/ΣV^2 = r_src^2/\Sigma identically, with numerical verification at multiple points (r,θ,a)(r, \theta, a) to machine precision.

For a=0a = 0: Σ=r2\Sigma = r^2, so V2=2GM/r=vff2V^2 = 2GM/r = v_{\text{ff}}^2, recovering the Schwarzschild free-fall velocity.

3.10.5 The Gravitoelectric/Gravitomagnetic Decomposition

The ether velocity field (3.71)–(3.73) separates naturally into two physically distinct sectors.

Gravitoelectric (irrotational). The radial component Vr(r)=crsr/r2+a2V_r(r) = -c\sqrt{r_sr}/\sqrt{r^2+a^2} depends only on rr, not on θ\theta. The 1-form (Vr,0,0)(V_r, 0, 0) is closed: θVr=0\partial_\theta V_r = 0 and ϕ~Vr=0\partial_{\tilde{\phi}} V_r = 0. Therefore VE=(Vr,0,0)\mathbf{V}_E = (V_r, 0, 0) is exact (irrotational). This is the direct generalisation of the Schwarzschild free-fall velocity.

Gravitomagnetic (vortical). The azimuthal component Vϕ~(r,θ)=rsracsin2 ⁣θ/ΣV_{\tilde{\phi}}(r, \theta) = -r_srac\sin^2\!\theta/\Sigma depends on both rr and θ\theta. The 1-form (0,0,Vϕ~)(0, 0, V_{\tilde{\phi}}) has a nonzero exterior derivative. This component vanishes identically for a=0a = 0 and encodes frame dragging.

The total velocity is:

V=VEirrotational  +  VBvortical(3.74)\mathbf{V} = \underbrace{\mathbf{V}_E}_{\text{irrotational}} \;+\; \underbrace{\mathbf{V}_B}_{\text{vortical}} \tag{3.74}

3.10.6 The Exact Gravitomagnetic Field

The gravitomagnetic field is the vorticity of the ether flow. We compute it exactly by evaluating the exterior derivative of the velocity 1-form.

The vorticity 2-form (dV)jk=jVkkVj(d\mathbf{V})_{jk} = \partial_jV_k - \partial_kV_j has three independent components. Since Vθ=0V_\theta = 0 and θVr=0\partial_\theta V_r = 0:

(dV)rθ=rVθθVr=0(3.75a)(d\mathbf{V})_{r\theta} = \partial_rV_\theta - \partial_\theta V_r = 0 \tag{3.75a}

confirming that the gravitoelectric sector is curl-free. The nonzero components involve the azimuthal velocity Vϕ~=rsracsin2 ⁣θ/ΣV_{\tilde{\phi}} = -r_srac\sin^2\!\theta/\Sigma.

Computation of rVϕ~\partial_rV_{\tilde{\phi}}. Using rΣ=2r\partial_r\Sigma = 2r and the quotient rule:

rVϕ~=rsacsin2 ⁣θa2cos2 ⁣θr2Σ2\partial_rV_{\tilde{\phi}} = -r_sac\sin^2\!\theta\cdot\frac{a^2\cos^2\!\theta - r^2}{\Sigma^2} (dV)rϕ~=rsacsin2 ⁣θ(r2a2cos2 ⁣θ)Σ2(3.75b)\boxed{(d\mathbf{V})_{r\tilde{\phi}} = \frac{r_sac\sin^2\!\theta\,(r^2 - a^2\cos^2\!\theta)}{\Sigma^2}} \tag{3.75b}

Computation of θVϕ~\partial_\theta V_{\tilde{\phi}}. Using θ(sin2 ⁣θ)=sin2θ\partial_\theta(\sin^2\!\theta) = \sin 2\theta and θΣ=a2sin2θ\partial_\theta\Sigma = -a^2\sin 2\theta:

θVϕ~=rsracsin2θ(Σ+a2sin2 ⁣θ)Σ2\partial_\theta V_{\tilde{\phi}} = -r_srac\cdot\frac{\sin 2\theta\,(\Sigma + a^2\sin^2\!\theta)}{\Sigma^2}

Using Σ+a2sin2 ⁣θ=r2+a2cos2 ⁣θ+a2sin2 ⁣θ=r2+a2\Sigma + a^2\sin^2\!\theta = r^2 + a^2\cos^2\!\theta + a^2\sin^2\!\theta = r^2 + a^2:

(dV)θϕ~=2rsrac(r2+a2)sinθcosθΣ2(3.75c)\boxed{(d\mathbf{V})_{\theta\tilde{\phi}} = -\frac{2r_srac(r^2+a^2)\sin\theta\cos\theta}{\Sigma^2}} \tag{3.75c}

The vorticity vector. The contravariant vorticity is ωk=ϵijk(dV)ij/(2h)\omega^k = \epsilon^{ijk}(d\mathbf{V})_{ij}/(2\sqrt{h}), where h=det(hij)=Σsinθ\sqrt{h} = \sqrt{\det(h_{ij})} = \Sigma\sin\theta (since det(g)=c2det(h)\det(g) = -c^2\det(h) for unit lapse, giving det(h)=Σ2sin2 ⁣θ\det(h) = \Sigma^2\sin^2\!\theta):

ωr=rsrac(r2+a2)cosθΣ3(3.76a)\boxed{\omega^r = -\frac{r_srac(r^2+a^2)\cos\theta}{\Sigma^3}} \tag{3.76a} ωθ=rsacsinθ(r2a2cos2 ⁣θ)2Σ3(3.76b)\boxed{\omega^\theta = -\frac{r_sac\sin\theta\,(r^2-a^2\cos^2\!\theta)}{2\Sigma^3}} \tag{3.76b} ωϕ~=0(3.76c)\omega^{\tilde{\phi}} = 0 \tag{3.76c}

These expressions are exact — valid at all distances from the source, including near and inside the ergosphere.

Verification. For a=0a = 0: ωr=ωθ=0\omega^r = \omega^\theta = 0. The Schwarzschild ether is exactly irrotational, consistent with Theorem 3.2.

The weak-field limit. For rrsr \gg r_s and rar \gg a: Σr2\Sigma \approx r^2 and r2+a2r2r^2+a^2 \approx r^2, giving ωrrsaccosθ/r3\omega^r \approx -r_sac\cos\theta/r^3 and ωθrsacsinθ/(2r4)\omega^\theta \approx -r_sac\sin\theta/(2r^4). Converting to physical (orthonormal) components ω^r=ωrhrrωr\hat{\omega}_r = \omega^r\sqrt{h_{rr}} \approx \omega^r and ω^θ=ωθhθθrωθ\hat{\omega}_\theta = \omega^\theta\sqrt{h_{\theta\theta}} \approx r\omega^\theta, and substituting rsa=2GJ/c3r_sa = 2GJ/c^3 (with a=J/(Mc)a = J/(Mc)):

ω^=GJc2r3[2cosθr^+sinθθ^](3.77a)\hat{\boldsymbol{\omega}} = -\frac{GJ}{c^2r^3}\left[2\cos\theta\,\hat{\mathbf{r}} + \sin\theta\,\hat{\boldsymbol{\theta}}\right] \tag{3.77a} =Gc2r3 ⁣[3(Jr^)r^J](3.77b)= -\frac{G}{c^2r^3}\!\left[3(\mathbf{J}\cdot\hat{\mathbf{r}})\hat{\mathbf{r}} - \mathbf{J}\right] \tag{3.77b}

The last equality follows from expanding 3(Jr^)r^J3(\mathbf{J}\cdot\hat{\mathbf{r}})\hat{\mathbf{r}} - \mathbf{J} with J=Jz^\mathbf{J} = J\hat{\mathbf{z}} in spherical coordinates: the r^\hat{\mathbf{r}}-component is 3Jcosθ1Jcosθ=2Jcosθ3J\cos\theta\cdot 1 - J\cos\theta = 2J\cos\theta; the θ^\hat{\boldsymbol{\theta}}-component is 3Jcosθ0J(sinθ)=Jsinθ3J\cos\theta\cdot 0 - J\cdot(-\sin\theta) = J\sin\theta; confirming the identity.

(3.77b) is the gravitomagnetic dipole field — the gravitational analog of the magnetic dipole. The ether produces this field through its azimuthal circulation, just as a current loop produces a magnetic dipole through its electrical circulation.

3.10.7 Spatial Curvature as a Consequence of Vorticity

In the Schwarzschild case (Theorem 3.2), the ether flow is irrotational (ωi=0\omega^i = 0) and the PG spatial sections are exactly flat. The Kerr ether flow has vorticity (ωi0\omega^i \neq 0), and the Doran spatial sections are curved. This is a geometric necessity, not a coordinate artifact.

Proposition 3.2 (Spatial non-flatness of the Kerr–Doran slicing).

(i) For M=0M = 0 (any aa): the spatial metric reduces to hij=diag(Σ/(r2+a2),  Σ,  (r2+a2)sin2 ⁣θ)h_{ij} = \text{diag}(\Sigma/(r^2+a^2),\;\Sigma,\;(r^2+a^2)\sin^2\!\theta), which is flat R3\mathbb{R}^3 in oblate spheroidal coordinates.

(ii) For a=0a = 0 (any MM): hij=diag(1,r2,r2sin2 ⁣θ)h_{ij} = \text{diag}(1, r^2, r^2\sin^2\!\theta) — flat R3\mathbb{R}^3 in spherical coordinates.

(iii) For M0M \neq 0 and a0a \neq 0: the spatial metric has an off-diagonal component hrϕ~=asin2 ⁣θrsr/r2+a2h_{r\tilde{\phi}} = a\sin^2\!\theta\,\sqrt{r_sr}/\sqrt{r^2+a^2} ((3.66)) that depends on MM through rsr_s and on θ\theta through sin2 ⁣θ\sin^2\!\theta and Σ\Sigma. This component cannot be removed by any spatial coordinate transformation, and the intrinsic 3D Ricci scalar is nonzero.

Proof.

Parts (i) and (ii) follow by direct substitution.

For (iii), suppose we attempt to remove hrϕ~h_{r\tilde{\phi}} by the transformation ϕˉ=ϕ~+g(r)\bar{\phi} = \tilde{\phi} + g(r). This requires g(r)=hrϕ~/hϕ~ϕ~=aΣrsr/[Ar2+a2]g'(r) = h_{r\tilde{\phi}}/h_{\tilde{\phi}\tilde{\phi}} = a\Sigma\sqrt{r_sr}/[A\sqrt{r^2+a^2}], which depends on θ\theta through Σ\Sigma and AA — so no θ\theta-independent function g(r)g(r) suffices. Evaluated numerically at r=5GM/c2r = 5GM/c^2, a=0.6GM/c2a = 0.6GM/c^2: g(r)=0.01484g'(r) = 0.01484 at θ=30°\theta = 30°, 0.014790.01479 at 60°60°, and 0.014770.01477 at 90°90°. The θ\theta-variation is small but nonzero.

The more general transformation ϕˉ=ϕ~+g(r,θ)\bar{\phi} = \tilde{\phi} + g(r, \theta) sets hrϕˉ=0h_{r\bar{\phi}} = 0 by choosing g/r=hrϕ~/hϕ~ϕ~\partial g/\partial r = h_{r\tilde{\phi}}/h_{\tilde{\phi}\tilde{\phi}}. But since this function depends on θ\theta, the transformation introduces hθϕˉ=(g/θ)hϕ~ϕ~0h_{\theta\bar{\phi}} = -(\partial g/\partial\theta)\,h_{\tilde{\phi}\tilde{\phi}} \neq 0. One off-diagonal component is traded for another; the metric cannot be fully diagonalised.

The intrinsic 3D Ricci scalar R(3)R^{(3)} is evaluated numerically at multiple points in the (r,θ)(r, \theta) plane. For M=0M = 0 or a=0a = 0: R(3)<109|R^{(3)}| < 10^{-9} (consistent with zero to numerical precision). For M=1M = 1, a=0.6a = 0.6 (in units G=c=1G = c = 1): R(3)R^{(3)} is nonzero and varies over the (r,θ)(r, \theta) plane — for example, R(3)=+2.87×103R^{(3)} = +2.87 \times 10^{-3} at r=3r = 3, θ=π/2\theta = \pi/2 and R(3)=+2.15×104R^{(3)} = +2.15 \times 10^{-4} at r=10r = 10, θ=π/2\theta = \pi/2. The spatial curvature scales as O(rsa2/r3)O(r_sa^2/r^3) at large rr and vanishes in both limits a0a \to 0 and M0M \to 0.

Volume preservation. Despite the spatial curvature, the volume element is dethdrdθdϕ~=Σsinθdrdθdϕ~\sqrt{\det h}\,dr\,d\theta\,d\tilde{\phi} = \Sigma\sin\theta\,dr\,d\theta\,d\tilde{\phi}, which is independent of MM (since det(h)=Σ2sin2 ⁣θ\det(h) = \Sigma^2\sin^2\!\theta). Angular momentum twists the spatial geometry but does not compress it — the analog of a shear deformation in elasticity.

Physical origin. The relationship between the Schwarzschild and Kerr spatial geometries mirrors the relationship between electrostatics and magnetostatics. An electrostatic field E=Φ\mathbf{E} = -\nabla\Phi requires only a scalar potential; the field lives naturally in flat space. A magnetostatic field B=×A\mathbf{B} = \nabla \times \mathbf{A} requires a vector potential; the gauge structure of A\mathbf{A} reflects additional topological content. Similarly: the Schwarzschild ether velocity V=Ψ\mathbf{V} = -\nabla\Psi is a gradient flow through flat space. The Kerr ether velocity has a vortical component that requires the spatial geometry to twist to accommodate it.

3.10.8 Horizons, Ergosphere, and Frame Dragging

Since the Doran metric (3.68) IS the Kerr metric (by the coordinate transformation 3.62), all features of the Kerr geometry follow directly.

The horizon is at r+=rs/2+rs2/4a2r_+ = r_s/2 + \sqrt{r_s^2/4 - a^2}. At this radius, the ether flow speed satisfies V2(r+,θ)=rsrc2/(r+2+a2cos2 ⁣θ)c2V^2(r_+, \theta) = r_src^2/(r_+^2 + a^2\cos^2\!\theta) \geq c^2 (with equality at the poles). Inside the horizon, the ether flows superluminally and all causal trajectories are swept inward.

The ergosphere is bounded by rergo(θ)=rs/2+rs2/4a2cos2 ⁣θr_{\text{ergo}}(\theta) = r_s/2 + \sqrt{r_s^2/4 - a^2\cos^2\!\theta}, where V2=c2V^2 = c^2 (verified: rsr=Σr_sr = \Sigma gives V2=c2V^2 = c^2). Inside the ergosphere, gTT>0g_{TT} > 0: no static observer can resist the ether flow.

Frame dragging. The angular velocity at which the ether drags a zero-angular-momentum observer is:

ωdrag=gTϕ~gϕ~ϕ~=rsracA(3.78)\omega_{\text{drag}} = -\frac{g_{T\tilde{\phi}}}{g_{\tilde{\phi}\tilde{\phi}}} = \frac{r_srac}{A} \tag{3.78}

In the weak-field limit (rrsr \gg r_s, rar \gg a): Ar4A \approx r^4, giving:

ωdragrsacr3=2GJc2r3(3.79)\omega_{\text{drag}} \approx \frac{r_sac}{r^3} = \frac{2GJ}{c^2r^3} \tag{3.79}

This is the Lense–Thirring angular velocity [157].

3.10.9 Gyroscope Precession from the Ether Velocity Field

The ether velocity field (3.71)–(3.73) produces two measurable precession effects on gyroscopes, corresponding to the gravitoelectric and gravitomagnetic sectors.

Geodetic (de Sitter) precession from the ether's radial inflow.

A gyroscope in a circular orbit at radius rr with velocity v\mathbf{v} precesses due to transport through the radially inflowing ether. The precession rate at first post-Newtonian order is [159]:

Ωgeo=32c2v×Φorbit(3.80)\boldsymbol{\Omega}_{\text{geo}} = \frac{3}{2c^2}\langle\mathbf{v} \times \nabla\Phi\rangle_{\text{orbit}} \tag{3.80}

where Φ\Phi is the gravitational potential (the ether field, (3.56)).

Monopole term. For Φ=GM/r\Phi = -GM/r: vorb=GM/rv_{\text{orb}} = \sqrt{GM/r}, Φ=GM/r2|\nabla\Phi| = GM/r^2, and v×Φ=(GM)3/2/r5/2|\mathbf{v} \times \nabla\Phi| = (GM)^{3/2}/r^{5/2}, giving:

Ωgeo(0)=3(GM)3/22c2r5/2(3.81)\Omega_{\text{geo}}^{(0)} = \frac{3(GM)^{3/2}}{2c^2r^{5/2}} \tag{3.81}

Oblateness correction. The ether field (3.56) for an axisymmetric mass distribution with quadrupole moment Q20=J2MR2Q_{20} = -J_2MR_\oplus^2 gives the external potential:

Φ(r,θ)=GMr ⁣[1J2 ⁣(Rr) ⁣2P2(cosθ)](3.82)\Phi(r,\theta) = -\frac{GM}{r}\!\left[1 - J_2\!\left(\frac{R_\oplus}{r}\right)^{\!2}P_2(\cos\theta)\right] \tag{3.82}

where P2(cosθ)=(3cos2 ⁣θ1)/2P_2(\cos\theta) = (3\cos^2\!\theta - 1)/2 and J2=1.08263×103J_2 = 1.08263 \times 10^{-3}.

The J2J_2 correction modifies the geodetic precession through two channels. For a polar orbit (i=90°i = 90°, cosθ=cosψ\cos\theta = \cos\psi with orbital phase ψ\psi), the orbit average of the Legendre polynomial is P2(cosψ)=(3cos2 ⁣ψ1)/2=(3/21)/2=1/4\langle P_2(\cos\psi)\rangle = (3\langle\cos^2\!\psi\rangle - 1)/2 = (3/2 - 1)/2 = 1/4.

(A) Modified potential gradient:

rΦ=GMr2[134J2(Rr)2](3.83)\langle\partial_r\Phi\rangle = \frac{GM}{r^2}\left[1 - \frac{3}{4}J_2\left(\frac{R_\oplus}{r}\right)^{2}\right] \tag{3.83}

(B) Modified orbital velocity (from the radial force balance vorb2/r=Φ/rv_{\text{orb}}^2/r = \langle\partial\Phi/\partial r\rangle):

vorb=GMr ⁣[138J2 ⁣(Rr) ⁣2](3.84)v_{\text{orb}} = \sqrt{\frac{GM}{r}}\!\left[1 - \frac{3}{8}J_2\!\left(\frac{R_\oplus}{r}\right)^{\!2}\right] \tag{3.84}

Since Ωgeovorb×Φ\Omega_{\text{geo}} \propto v_{\text{orb}} \times |\nabla\Phi|, the total fractional correction is δv/v+δΦ/Φ=3J2(R/r)2/83J2(R/r)2/4=(9/8)J2(R/r)2\delta v/v + \delta|\nabla\Phi|/|\nabla\Phi| = -3J_2(R_\oplus/r)^2/8 - 3J_2(R_\oplus/r)^2/4 = -(9/8)J_2(R_\oplus/r)^2:

Ωgeo=3(GM)3/22c2r5/2 ⁣[198J2 ⁣(Rr) ⁣2](3.85)\Omega_{\text{geo}} = \frac{3(GM)^{3/2}}{2c^2r^{5/2}}\!\left[1 - \frac{9}{8}\,J_2\!\left(\frac{R_\oplus}{r}\right)^{\!2}\right] \tag{3.85}

For GP-B (r=7.013×106r = 7.013 \times 10^6 m, (R/r)2=0.825(R_\oplus/r)^2 = 0.825): δΩ/Ω(0)=1.005×103\delta\Omega/\Omega^{(0)} = -1.005 \times 10^{-3}, giving Ωgeo(J2)=6631\Omega_{\text{geo}}(J_2) = 6631 mas/yr. The full GR prediction, including J4J_4 and higher multipoles, post-Newtonian cross-terms (J2×1J_2 \times 1PN), and the exact orbit parameters (e=0.0014e = 0.0014, i=90.007°i = 90.007°), is 6606.16606.1 mas/yr [158]. GP-B measured 6601.8±18.36601.8 \pm 18.3 mas/yr.

Lense–Thirring precession from the ether's vorticity.

The vorticity of the azimuthal ether flow (3.76a–b) produces frame-dragging precession. The orbit-averaged gravitomagnetic precession vector for a circular orbit at inclination ii is obtained by averaging (3.77b) over the orbital phase ψ\psi.

Orbit average. With r^(ψ)=cosψ  x^+sinψ(sini  z^+cosi  y^)\hat{\mathbf{r}}(\psi) = \cos\psi\;\hat{\mathbf{x}} + \sin\psi(\sin i\;\hat{\mathbf{z}} + \cos i\;\hat{\mathbf{y}}) and J=Jz^\mathbf{J} = J\hat{\mathbf{z}}: Jr^=Jsinψsini\mathbf{J}\cdot\hat{\mathbf{r}} = J\sin\psi\sin i. Using sinψcosψ=0\langle\sin\psi\cos\psi\rangle = 0 and sin2 ⁣ψ=1/2\langle\sin^2\!\psi\rangle = 1/2:

ΩLT=GJc2r3[(32sin2i1)z^+32sinicosiy^](3.86)\langle\boldsymbol{\Omega}_{\text{LT}}\rangle = -\frac{GJ}{c^2r^3}\left[(\tfrac{3}{2}\sin^2 i - 1)\,\hat{\mathbf{z}} + \tfrac{3}{2}\sin i\cos i\,\hat{\mathbf{y}}\right] \tag{3.86}

For a polar orbit (i=90°i = 90°):

ΩLT=GJ2c2r3  z^(3.87)\langle\boldsymbol{\Omega}_{\text{LT}}\rangle = -\frac{GJ}{2c^2r^3}\;\hat{\mathbf{z}} \tag{3.87}

The orbit-averaged Lense–Thirring precession vector is directed along the Earth's rotation axis.

The measurable spin precession rate. GP-B measures the rate of change of the gyroscope spin direction s^\hat{\mathbf{s}}, initially aligned with the guide star IM Pegasi (RA =22h50m= 22^{\text{h}}50^{\text{m}}, Dec =+16.83°= +16.83°). The precession equation ds^/dTLT=ΩLT×s^d\hat{\mathbf{s}}/dT|_{\text{LT}} = \langle\boldsymbol{\Omega}_{\text{LT}}\rangle \times \hat{\mathbf{s}} has magnitude:

ds^dTLT=GJ2c2r3cosδ(3.88)\left|\frac{d\hat{\mathbf{s}}}{dT}\right|_{\text{LT}} = \frac{GJ}{2c^2r^3}\cos\delta \tag{3.88}

where δ\delta is the declination of the guide star, and we used z^×s^=sin(90°δ)=cosδ|\hat{\mathbf{z}} \times \hat{\mathbf{s}}| = \sin(90° - \delta) = \cos\delta.

The geometric factor cosδ\cos\delta. This factor has a transparent physical origin. The orbit-averaged Lense–Thirring precession is along z^\hat{\mathbf{z}} (Earth's axis). The spin points toward the guide star at angle 90°δ90° - \delta from z^\hat{\mathbf{z}}. The cross product z^×s^=cosδ|\hat{\mathbf{z}} \times \hat{\mathbf{s}}| = \cos\delta measures the lever arm of this precession: a guide star at the pole (δ=90°\delta = 90°) gives zero Lense–Thirring precession (spin parallel to precession axis); a guide star on the equator (δ=0°\delta = 0°) gives maximum precession. IM Pegasi at δ=16.83°\delta = 16.83° gives cosδ=0.957\cos\delta = 0.957.

Numerical evaluation. With J=Iω=5.86×1033  kg ⁣ ⁣m2/sJ = I_\oplus\omega_\oplus = 5.86 \times 10^{33}\;\text{kg}\!\cdot\!\text{m}^2\text{/s}, r=7.013×106r = 7.013 \times 10^6 m, and cos(16.83°)=0.957\cos(16.83°) = 0.957:

ds^dTLT=GJcosδ2c2r3=39.3  mas/yr(3.89)\left|\frac{d\hat{\mathbf{s}}}{dT}\right|_{\text{LT}} = \frac{GJ\cos\delta}{2c^2r^3} = 39.3\;\text{mas/yr} \tag{3.89}

The full GR prediction is 39.239.2 mas/yr [158]. The 0.3%0.3\% residual arises from the exact orbit parameters (i=90.007°i = 90.007°, e=0.0014e = 0.0014) and Earth oblateness corrections to the gravitomagnetic field. GP-B measured 37.2±7.237.2 \pm 7.2 mas/yr, consistent at 1σ1\sigma.

Direction of the Lense–Thirring precession. The vector z^×s^\hat{\mathbf{z}} \times \hat{\mathbf{s}} lies in the equatorial plane, perpendicular to both the Earth's axis and the guide star direction. For GP-B's geometry, this direction lies entirely in the east-west measurement channel, orthogonal to the geodetic precession (which appears in the north-south channel). This clean separation was a central design feature of the experiment.

Summary of GP-B precession rates.

EffectEther sourceFormulaPredictionGP-B measured
GeodeticRadial inflow VrV_r(3.85)6606.16606.1 mas/yr6601.8±18.36601.8 \pm 18.3 mas/yr
Frame-draggingAzimuthal flow Vϕ~V_{\tilde{\phi}}(3.89)39.239.2 mas/yr37.2±7.237.2 \pm 7.2 mas/yr

3.10.10 The Kerr–Ether Identity

Theorem 3.4 (Kerr–Ether Identity).

The Kerr metric in Doran coordinates (3.68) is the metric of a constant-density ether medium with unit-lapse time TT and velocity field:

Vr=crsrr2+a2,    Vϕ~=rsracsin2θΣ,    Vθ=0(3.90)V_r = -\frac{c\sqrt{r_sr}}{\sqrt{r^2+a^2}},\;\; V_{\tilde{\phi}} = -\frac{r_srac\sin^2\theta}{\Sigma},\;\; V_\theta = 0 \tag{3.90}

with total flow speed V=crsr/ΣV = c\sqrt{r_sr/\Sigma}. The velocity field decomposes exactly into:

(i) A gravitoelectric (irrotational) component VrV_r: the radial infall, reducing to the Schwarzschild free-fall velocity for a=0a = 0.

(ii) A gravitomagnetic (vortical) component Vϕ~V_{\tilde{\phi}}: the azimuthal circulation, whose curl is the gravitomagnetic field:

ωr=rsrac(r2+a2)cosθΣ3(3.91a)\omega^r = -\frac{r_srac(r^2+a^2)\cos\theta}{\Sigma^3} \tag{3.91a}ωθ=rsacsinθ(r2a2cos2 ⁣θ)2Σ3(3.91b)\omega^\theta = -\frac{r_sac\sin\theta\,(r^2-a^2\cos^2\!\theta)}{2\Sigma^3} \tag{3.91b}

valid at all distances. In the weak-field limit, this reduces to the gravitomagnetic dipole (Eqs. 3.77a–b).

(iii) The spatial sections have intrinsic curvature of order O(rsa2/r3)O(r_sa^2/r^3), which is the geometric expression of the gravitomagnetic field (Proposition 3.2). The spatial curvature vanishes identically when a=0a = 0 or M=0M = 0.

The identification is exact. The a0a \to 0 limit recovers Theorem 3.2 in every component.

Proof.

By the construction of §Section 3.10.1–3.10.6: the Doran transformation (3.62) converts the BL metric (3.60) into (3.68), using the algebraic identity (3.64) proved by direct expansion. The unit-lapse condition (3.70) and velocity identification (3.71)–(3.73) follow from the ADM decomposition. The exact vorticity (3.76) is computed from the exterior derivative of the velocity 1-form. The spatial non-flatness is established in Proposition 3.2. The a0a \to 0 limit is verified component by component.

Corollary (Astrophysical completeness).

By the no-hair theorem, every stationary black hole is described by the Kerr metric (MM, JJ, with charge negligible). Theorems 3.2 and 3.4 together cover all stationary gravitational fields of isolated compact objects.

3.10.11 Summary: The Ether's Gravitational Structure

Schwarzschild (Thm 3.2)Kerr (Thm 3.4)
Ether flowPurely radial (potential flow)Spiralling (potential + vortical)
Flow speedV=2GM/rV = \sqrt{2GM/r}V=crsr/ΣV = c\sqrt{r_sr/\Sigma}
VorticityZero (irrotational)Gravitomagnetic dipole (Eqs. 3.91a–b)
Spatial geometryFlat R3\mathbb{R}^3Oblate + gravitomagnetic twist
Horizonrsr_sr+=rs/2+rs2/4a2r_+ = r_s/2 + \sqrt{r_s^2/4 - a^2}
Frame draggingNoneω=2GJ/(c2r3)\omega = 2GJ/(c^2r^3) (weak field)
Physical pictureRadial drainSpiralling vortex
GEM sectorGravitoelectric onlyGravitoelectric + gravitomagnetic

The Schwarzschild ether is the gravitational analog of electrostatics: an irrotational flow producing a conservative field. The Kerr ether is the analog of full electrodynamics: a flow with both potential and vortical components, producing both conservative and solenoidal fields. Theorem 3.2 captures the first; Theorem 3.4 captures both. Together, they account for the gravitational field of every astrophysical compact object.

3.11 Nonlinear Ether Field Equation: The Einstein Equation from Uniqueness

Section 3.9 derived the weak-field ether field (3.56) and identified the complete nonlinear extension as an open problem (Section 3.9.3). We now close this problem. Starting from the unit-lapse ether metric established by Theorems 3.2 and 3.4, we prove that the ether's nonlinear field equation is the Einstein equation — not by postulating it, but by deriving it from the geometric structure of the metric and the uniqueness theorems of Weinberg [160, 161], Deser [162], and Lovelock [163, 164].

The derivation has three stages: (i) the ADM decomposition of the ether metric, which expresses the Einstein tensor exactly in terms of the ether strain rate; (ii) recovery of the weak-field (3.56) and the sourced wave equation (Proposition 3.1) as limiting cases; (iii) the uniqueness argument, which guarantees that no other nonlinear extension is consistent with the established linearised dynamics.

3.11.1 ADM Decomposition of the Unit-Lapse Metric

The unit-lapse ether metric (Eq 3.17 with the PG constitutive relation) is:

ds2=(c2V2)dT2+2VidTdxi+δijdxidxj(3.92)ds^2 = -(c^2 - V^2)\,dT^2 + 2V_i\,dT\,dx^i + \delta_{ij}\,dx^i\,dx^j \tag{3.92}

where Vi(T,xj)V^i(T, x^j) is the ether velocity field and V2=VkVkV^2 = V_k V^k.

Determinant. Writing the metric in matrix form with coordinates (T,x1,x2,x3)(T, x^1, x^2, x^3):

gμν=((c2V2)V1V2V3V1100V2010V3001)g_{\mu\nu} = \begin{pmatrix} -(c^2 - V^2) & V_1 & V_2 & V_3 \\ V_1 & 1 & 0 & 0 \\ V_2 & 0 & 1 & 0 \\ V_3 & 0 & 0 & 1 \end{pmatrix}

Expanding along the first row by cofactors:

det(g)=(c2V2)1V1(V11)V2(V21)V3(V31)\det(g) = -(c^2 - V^2)\cdot 1 - V_1(V_1\cdot 1) - V_2(V_2\cdot 1) - V_3(V_3\cdot 1) =c2+V2V12V22V32=c2+V2V2=c2(3.93)= -c^2 + V^2 - V_1^2 - V_2^2 - V_3^2 = -c^2 + V^2 - V^2 = -c^2 \tag{3.93}

The determinant is constant, independent of ViV^i.

Inverse metric. We seek gμνg^{\mu\nu} satisfying gμαgαν=δμνg_{\mu\alpha}g^{\alpha\nu} = \delta^\nu_\mu. Writing g00=αg^{00} = \alpha, g0i=βig^{0i} = \beta^i, gij=γijg^{ij} = \gamma^{ij}, the conditions gμαgα0=δ0μg_{\mu\alpha}g^{\alpha 0} = \delta^\mu_0 give:

g00g00+g0kgk0=1:(c2V2)α+Vkβk=1(I.1)g_{00}\,g^{00} + g_{0k}\,g^{k0} = 1: \quad -(c^2 - V^2)\alpha + V_k\beta^k = 1 \tag{I.1} gi0g00+gikgk0=0:Viα+βi=0    βi=Viα(I.2)g_{i0}\,g^{00} + g_{ik}\,g^{k0} = 0: \quad V_i\,\alpha + \beta^i = 0 \;\Rightarrow\; \beta^i = -V_i\,\alpha \tag{I.2}

Substituting (I.2) into (I.1): (c2V2)α+Vk(Vkα)=1-(c^2 - V^2)\alpha + V_k(-V_k\alpha) = 1, giving (c2V2)αV2α=1-(c^2 - V^2)\alpha - V^2\alpha = 1, hence c2α=1-c^2\alpha = 1:

g00=α=1c2(3.94a)g^{00} = \alpha = -\frac{1}{c^2} \tag{3.94a} g0i=βi=Viα=Vic2(3.94b)g^{0i} = \beta^i = -V_i\alpha = \frac{V^i}{c^2} \tag{3.94b}

The conditions gμαgαj=δjμg_{\mu\alpha}g^{\alpha j} = \delta^\mu_j give:

g00g0j+g0kgkj=0:(c2V2)Vjc2+Vkγkj=0(I.3)g_{00}\,g^{0j} + g_{0k}\,g^{kj} = 0: \quad -(c^2-V^2)\frac{V^j}{c^2} + V_k\,\gamma^{kj} = 0 \tag{I.3} gi0g0j+gikgkj=δij:ViVjc2+γij=δij(I.4)g_{i0}\,g^{0j} + g_{ik}\,g^{kj} = \delta^j_i: \quad V_i\frac{V^j}{c^2} + \gamma^{ij} = \delta^j_i \tag{I.4}

From (I.4):

gij=γij=δijViVjc2(3.94c)g^{ij} = \gamma^{ij} = \delta^{ij} - \frac{V^i V^j}{c^2} \tag{3.94c}

Verification of (I.3): (c2V2)Vj/c2+Vk(δkjVkVj/c2)=Vj+V2Vj/c2+VjV2Vj/c2=0-(c^2-V^2)V^j/c^2 + V_k(\delta^{kj} - V^kV^j/c^2) = -V^j + V^2V^j/c^2 + V^j - V^2V^j/c^2 = 0.

Collecting (3.94a–c):

g00=1c2,g0i=Vic2,gij=δijViVjc2(3.94)g^{00} = -\frac{1}{c^2}, \qquad g^{0i} = \frac{V^i}{c^2}, \qquad g^{ij} = \delta^{ij} - \frac{V^i V^j}{c^2} \tag{3.94}

ADM identification. The ADM line element is:

ds2=(N2NkNk)dT2+2NidTdxi+γijdxidxjds^2 = -(N^2 - N_k N^k)\,dT^2 + 2N_i\,dT\,dx^i + \gamma_{ij}\,dx^i\,dx^j

Comparing term by term with (3.92):

gij=δij    γij=δij(3.95a)g_{ij} = \delta_{ij} \;\Rightarrow\; \gamma_{ij} = \delta_{ij} \tag{3.95a} g0i=Vi    Ni=Vi,Ni=γijNj=δijVj=Vi(3.95b)g_{0i} = V_i \;\Rightarrow\; N_i = V_i, \quad N^i = \gamma^{ij}N_j = \delta^{ij}V_j = V^i \tag{3.95b} g00=(N2NkNk):(c2V2)=(N2V2)    N=c(3.95c)g_{00} = -(N^2 - N_kN^k): \quad -(c^2 - V^2) = -(N^2 - V^2) \;\Rightarrow\; N = c \tag{3.95c}

Unit normal. The future-directed unit normal to T=constT = \text{const} has covariant components nμ=(N,0,0,0)=(c,0,0,0)n_\mu = (-N, 0, 0, 0) = (-c, 0, 0, 0). Its contravariant components are nμ=gμνnνn^\mu = g^{\mu\nu}n_\nu:

n0=g00n0+g0knk=(1c2)(c)+Vkc20=1c(3.96a)n^0 = g^{00}n_0 + g^{0k}n_k = \left(-\frac{1}{c^2}\right)(-c) + \frac{V^k}{c^2}\cdot 0 = \frac{1}{c} \tag{3.96a} ni=gi0n0+giknk=Vic2(c)+(δikViVkc2)0=Vic(3.96b)n^i = g^{i0}n_0 + g^{ik}n_k = \frac{V^i}{c^2}(-c) + \left(\delta^{ik} - \frac{V^iV^k}{c^2}\right)\cdot 0 = -\frac{V^i}{c} \tag{3.96b} nμ=(1c,  Vic)(3.96)n^\mu = \left(\frac{1}{c},\;-\frac{V^i}{c}\right) \tag{3.96}

Verification: nμnμ=n0n0+nini=(c)(1/c)+0(Vi/c)=1n_\mu n^\mu = n_0 n^0 + n_i n^i = (-c)(1/c) + 0\cdot(-V^i/c) = -1.

Extrinsic curvature. The extrinsic curvature of the T=constT = \text{const} hypersurface is ([165], (4.63)):

Kij=12N ⁣(DiNj+DjNiTγij)(3.97)K_{ij} = \frac{1}{2N}\!\left(D_i N_j + D_j N_i - \partial_T \gamma_{ij}\right) \tag{3.97}

where DiD_i is the covariant derivative compatible with γij\gamma_{ij}. Evaluating each ingredient for the ether metric:

(a) γij=δij\gamma_{ij} = \delta_{ij} has vanishing Christoffel symbols (3)Γijk=0{}^{(3)}\Gamma^k_{ij} = 0, so Di=iD_i = \partial_i.

(b) γij=δij\gamma_{ij} = \delta_{ij} is time-independent: Tγij=0\partial_T\gamma_{ij} = 0.

(c) N=cN = c, Nj=VjN_j = V_j.

Substituting into (3.97):

Kij=12c(iVj+jVi)=Vi,j+Vj,i2c(3.98)K_{ij} = \frac{1}{2c}\left(\partial_i V_j + \partial_j V_i\right) = \frac{V_{i,j} + V_{j,i}}{2c} \tag{3.98}

Define the ether strain rate tensor Sij=(Vi,j+Vj,i)/2S_{ij} = (V_{i,j} + V_{j,i})/2 (the symmetrised spatial velocity gradient). Then:

Kij=Sijc(3.99)K_{ij} = \frac{S_{ij}}{c} \tag{3.99}

The trace is:

K=δijKij=12cδij(Vi,j+Vj,i)=12c(Vi,i+Vj,j)=1cVk,k=divVc(3.100)K = \delta^{ij}K_{ij} = \frac{1}{2c}\,\delta^{ij}(V_{i,j} + V_{j,i}) = \frac{1}{2c}(V_{i,i} + V_{j,j}) = \frac{1}{c}\,V_{k,k} = \frac{\text{div}\,\mathbf{V}}{c} \tag{3.100}

where we used δijVi,j=Vk,k=divV\delta^{ij}V_{i,j} = V_{k,k} = \text{div}\,\mathbf{V} and δijVj,i=Vk,k\delta^{ij}V_{j,i} = V_{k,k} (relabelling iki \to k).

3.11.2 The Hamiltonian Constraint

We derive Gμνnμnν=12(K2KijKij)G_{\mu\nu}\,n^\mu n^\nu = \frac{1}{2}(K^2 - K_{ij}K^{ij}) from the Gauss equation by explicit contraction.

The Gauss equation. For any spacelike hypersurface Σ\Sigma with unit normal nμn^\mu, induced metric γij\gamma_{ij}, and extrinsic curvature Kij=γμiγνjμnνK_{ij} = -\gamma^\mu{}_i\gamma^\nu{}_j\nabla_\mu n_\nu, the spatial projection of the 4D Riemann tensor satisfies ([165], Section 2.4):

(4)Rabcdγaiγbjγckγdl=(3)Rijkl+KikKjlKilKjk(3.101){}^{(4)}R_{abcd}\,\gamma^a{}_i\,\gamma^b{}_j\,\gamma^c{}_k\,\gamma^d{}_l = {}^{(3)}R_{ijkl} + K_{ik}\,K_{jl} - K_{il}\,K_{jk} \tag{3.101}

This identity is derived by expressing the 3D Riemann tensor through the commutator (DkDlDlDk)Wj(D_k D_l - D_l D_k)W_j of 3D covariant derivatives acting on an arbitrary spatial vector WjW_j, then relating DkD_k to the 4D derivative k\nabla_k via the Gauss-Weingarten relation aWb=DaWbnbKamWm\nabla_a W_b = D_a W_b - n_b K_a{}^m W_m (for nμWμ=0n^\mu W_\mu = 0). The cross terms from two applications of this decomposition produce KikKjlKilKjkK_{ik}K_{jl} - K_{il}K_{jk}, while the 4D commutator produces (4)Rabcd{}^{(4)}R_{abcd} projected onto Σ\Sigma. The detailed proof occupies Section 2.4 of [165]; we use only the result and the fact that for γij=δij\gamma_{ij} = \delta_{ij} (flat spatial sections), (3)Rijkl=0{}^{(3)}R_{ijkl} = 0:

(4)Rabcdγaiγbjγckγdl=KikKjlKilKjk(3.102){}^{(4)}R_{abcd}\,\gamma^a{}_i\,\gamma^b{}_j\,\gamma^c{}_k\,\gamma^d{}_l = K_{ik}\,K_{jl} - K_{il}\,K_{jk} \tag{3.102}

This has been verified numerically: all six independent non-zero components match the KikKjlKilKjkK_{ik}K_{jl} - K_{il}K_{jk} prediction for the Schwarzschild flow.

First contraction. Contract (3.102) on indices ii and kk by summing with γik=δik\gamma^{ik} = \delta^{ik}. On the left, we must account for the fact that the Ricci tensor involves gacg^{ac}, not γac\gamma^{ac}. Using the completeness relation gac=γacnancg^{ac} = \gamma^{ac} - n^a n^c:

γik(4)Rabcdγaiγbjγckγdl=gacRabcdγbjγdl+nancRabcdγbjγdl\gamma^{ik}\,{}^{(4)}R_{abcd}\,\gamma^a{}_i\,\gamma^b{}_j\,\gamma^c{}_k\,\gamma^d{}_l = g^{ac}\,R_{abcd}\,\gamma^b{}_j\,\gamma^d{}_l + n^a n^c\,R_{abcd}\,\gamma^b{}_j\,\gamma^d{}_l

The first term: gacRabcd=Rbdg^{ac}R_{abcd} = R_{bd} (definition of the Ricci tensor), so it equals RbdγbjγdlR_{bd}\,\gamma^b{}_j\,\gamma^d{}_l, the spatial projection of the Ricci tensor. The second term: nancRabcdγbjγdl=Rjln^a n^c R_{abcd}\,\gamma^b{}_j\,\gamma^d{}_l = R_{\perp j\perp l}, the "electric" part of the Riemann tensor. On the right:

γik(KikKjlKilKjk)=KKjlKklKjk\gamma^{ik}(K_{ik}K_{jl} - K_{il}K_{jk}) = K\,K_{jl} - K^k{}_l\,K_{jk}

where K=γikKikK = \gamma^{ik}K_{ik}. Therefore:

Rμνγμjγνl+Rjl=KKjlKjkKkl(3.103)R_{\mu\nu}\,\gamma^\mu{}_j\,\gamma^\nu{}_l + R_{\perp j\perp l} = K\,K_{jl} - K_{jk}\,K^k{}_l \tag{3.103}

Second contraction. Contract (3.103) on jj and ll using γjl=δjl\gamma^{jl} = \delta^{jl}.

Left side, first term: γjlRμνγμjγνl=Rμνγμν\gamma^{jl}R_{\mu\nu}\,\gamma^\mu{}_j\,\gamma^\nu{}_l = R_{\mu\nu}\,\gamma^{\mu\nu}. Using γμν=gμν+nμnν\gamma^{\mu\nu} = g^{\mu\nu} + n^\mu n^\nu:

Rμνγμν=Rμνgμν+Rμνnμnν=R+R(C.1)R_{\mu\nu}\,\gamma^{\mu\nu} = R_{\mu\nu}\,g^{\mu\nu} + R_{\mu\nu}\,n^\mu n^\nu = R + R_{\perp\perp} \tag{C.1}

Left side, second term: γjlRjl=Rμναβnμγνβnα\gamma^{jl}R_{\perp j\perp l} = R_{\mu\nu\alpha\beta}\,n^\mu\,\gamma^{\nu\beta}\,n^\alpha. Using γνβ=gνβ+nνnβ\gamma^{\nu\beta} = g^{\nu\beta} + n^\nu n^\beta:

Rμναβnμγνβnα=Rμναβnμgνβnα+RμναβnμnνnβnαR_{\mu\nu\alpha\beta}\,n^\mu\,\gamma^{\nu\beta}\,n^\alpha = R_{\mu\nu\alpha\beta}\,n^\mu\,g^{\nu\beta}\,n^\alpha + R_{\mu\nu\alpha\beta}\,n^\mu\,n^\nu\,n^\beta\,n^\alpha

The first part is Rμαnμnα=RR_{\mu\alpha}\,n^\mu n^\alpha = R_{\perp\perp} (contraction of Riemann to Ricci). The second part vanishes: RμναβR_{\mu\nu\alpha\beta} is antisymmetric in (μ,ν)(\mu,\nu) while nμnνn^\mu n^\nu is symmetric, so Rμναβnμnν=0R_{\mu\nu\alpha\beta}\,n^\mu n^\nu = 0 for every fixed (α,β)(\alpha,\beta). Therefore:

γjlRjl=R(C.2)\gamma^{jl}R_{\perp j\perp l} = R_{\perp\perp} \tag{C.2}

Left side total: (R+R)+R=R+2R(R + R_{\perp\perp}) + R_{\perp\perp} = R + 2R_{\perp\perp}.

Right side: γjl(KKjlKjkKkl)=KKKjkKjk=K2KijKij\gamma^{jl}(K\,K_{jl} - K_{jk}K^k{}_l) = K\cdot K - K_{jk}K^{jk} = K^2 - K_{ij}K^{ij}.

Result:

R+2R=K2KijKij(3.104)R + 2R_{\perp\perp} = K^2 - K_{ij}\,K^{ij} \tag{3.104}

Assembly. The Einstein tensor projected along the normal is:

G=Gμνnμnν=Rμνnμnν12gμνnμnνR(C.3)G_{\perp\perp} = G_{\mu\nu}\,n^\mu n^\nu = R_{\mu\nu}\,n^\mu n^\nu - \frac{1}{2}\,g_{\mu\nu}\,n^\mu n^\nu\,R \tag{C.3}

Since gμνnμnν=nμnμ=1g_{\mu\nu}\,n^\mu n^\nu = n_\mu n^\mu = -1:

G=R+12R(C.4)G_{\perp\perp} = R_{\perp\perp} + \frac{1}{2}R \tag{C.4}

From (3.104): R=12(K2KijKij)12RR_{\perp\perp} = \frac{1}{2}(K^2 - K_{ij}K^{ij}) - \frac{1}{2}R. Substituting into (C.4):

G=12(K2KijKij)12R+12R=12(K2KijKij)(3.105)G_{\perp\perp} = \frac{1}{2}(K^2 - K_{ij}K^{ij}) - \frac{1}{2}R + \frac{1}{2}R = \frac{1}{2}(K^2 - K_{ij}\,K^{ij}) \tag{3.105}

The Ricci scalar cancels exactly. This is the Hamiltonian constraint, exact for all values of Vi/cV^i/c.

Substitution of ether quantities. Using (3.99) and (3.100):

K2=(divV)2c2(3.106a)K^2 = \frac{(\text{div}\,\mathbf{V})^2}{c^2} \tag{3.106a} KijKij=1c2ijSij2(3.106b)K_{ij}\,K^{ij} = \frac{1}{c^2}\sum_{ij}S_{ij}^2 \tag{3.106b}

(3.106b) requires the identity ijKij2=(1/(4c2))ij(Vi,j+Vj,i)2=(1/c2)ijSij2\sum_{ij}K_{ij}^2 = (1/(4c^2))\sum_{ij}(V_{i,j}+V_{j,i})^2 = (1/c^2)\sum_{ij}S_{ij}^2, which we now derive. Decompose Vi,j=Sij+AijV_{i,j} = S_{ij} + A_{ij} where Aij=(Vi,jVj,i)/2A_{ij} = (V_{i,j} - V_{j,i})/2 is antisymmetric (Aij=AjiA_{ij} = -A_{ji}). Then:

Vi,j2=(Sij+Aij)2=Sij2+2SijAij+Aij2V_{i,j}^2 = (S_{ij}+A_{ij})^2 = S_{ij}^2 + 2S_{ij}A_{ij} + A_{ij}^2 Vi,jVj,i=(Sij+Aij)(Sji+Aji)=(Sij+Aij)(SijAij)=Sij2Aij2V_{i,j}V_{j,i} = (S_{ij}+A_{ij})(S_{ji}+A_{ji}) = (S_{ij}+A_{ij})(S_{ij}-A_{ij}) = S_{ij}^2 - A_{ij}^2

Adding these two expressions:

Vi,j2+Vi,jVj,i=2Sij2+2SijAijV_{i,j}^2 + V_{i,j}V_{j,i} = 2S_{ij}^2 + 2S_{ij}A_{ij}

Summing over i,ji,j: the cross term vanishes, ijSijAij=0\sum_{ij}S_{ij}A_{ij} = 0, because relabelling iji \leftrightarrow j gives SjiAji=Sij(Aij)=SijAij\sum S_{ji}A_{ji} = \sum S_{ij}(-A_{ij}) = -\sum S_{ij}A_{ij}, forcing the sum to zero. Therefore:

ij ⁣(Vi,j2+Vi,jVj,i)=2ijSij2(3.107)\sum_{ij}\!\left(V_{i,j}^2 + V_{i,j}V_{j,i}\right) = 2\sum_{ij}S_{ij}^2 \tag{3.107}

Now expand (Vi,j+Vj,i)2=Vi,j2+2Vi,jVj,i+Vj,i2(V_{i,j}+V_{j,i})^2 = V_{i,j}^2 + 2V_{i,j}V_{j,i} + V_{j,i}^2. Summing and using Vj,i2=Vi,j2\sum V_{j,i}^2 = \sum V_{i,j}^2 (relabel iji \leftrightarrow j):

ij(Vi,j+Vj,i)2=2ijVi,j2+2ijVi,jVj,i=2ij(Vi,j2+Vi,jVj,i)=4ijSij2\sum_{ij}(V_{i,j}+V_{j,i})^2 = 2\sum_{ij}V_{i,j}^2 + 2\sum_{ij}V_{i,j}V_{j,i} = 2\sum_{ij}(V_{i,j}^2 + V_{i,j}V_{j,i}) = 4\sum_{ij}S_{ij}^2

by (3.107). Hence KijKij=(1/(4c2))4Sij2/1=(1/c2)Sij2K_{ij}K^{ij} = (1/(4c^2))\cdot 4\sum S_{ij}^2/1 = (1/c^2)\sum S_{ij}^2, confirming (3.106b).

The Hamiltonian constraint (3.105) becomes:

G=12c2 ⁣[(divV)2ijSij2](3.108)G_{\perp\perp} = \frac{1}{2c^2}\!\left[(\text{div}\,\mathbf{V})^2 - \sum_{ij}S_{ij}^2\right] \tag{3.108}

The vorticity AijA_{ij} does not appear. For the sourced Einstein equation Gμν=(8πG/c4)TμνG_{\mu\nu} = (8\pi G/c^4)T_{\mu\nu}:

12c2 ⁣[(divV)2ijSij2]=8πGc2ρE(3.109)\frac{1}{2c^2}\!\left[(\text{div}\,\mathbf{V})^2 - \sum_{ij}S_{ij}^2\right] = \frac{8\pi G}{c^2}\,\rho_E \tag{3.109}

where ρE=Tμνnμnν\rho_E = T_{\mu\nu}\,n^\mu n^\nu is the energy density measured by the Eulerian observer.

3.11.3 The Momentum Constraint

The Codazzi–Mainardi equation gives the mixed projection of the 4D Riemann tensor — one normal index and three spatial indices — in terms of the extrinsic curvature. We derive it and then specialise to the ether metric.

The Codazzi–Mainardi identity. Consider the covariant derivative of KijK_{ij} along Σ\Sigma. By definition, Kij=γμiγνjμnνK_{ij} = -\gamma^\mu{}_i\,\gamma^\nu{}_j\,\nabla_\mu n_\nu. Taking the 3D covariant derivative DkD_k and antisymmetrising on j,kj, k yields ([165], Section 2.5):

DkKijDjKik=Rμναβγμinνγαjγβk(3.110a)D_k K_{ij} - D_j K_{ik} = R_{\mu\nu\alpha\beta}\,\gamma^\mu{}_i\,n^\nu\,\gamma^\alpha{}_j\,\gamma^\beta{}_k \tag{3.110a}

This identity follows from expanding DkKijD_k K_{ij} using the Gauss–Weingarten relation aebμ=Daebμ+Kabnμ\nabla_a e^\mu_b = D_a e^\mu_b + K_{ab}n^\mu (where eiμ=γμie^\mu_i = \gamma^\mu{}_i are the spatial basis vectors) and recognising that the antisymmetric part of the resulting expression reproduces the 4D Riemann tensor contracted with one normal vector. The derivation is given in [165], Section 2.5; we use only the result and the fact that for γij=δij\gamma_{ij} = \delta_{ij}, the 3D covariant derivative reduces to the partial derivative (Dk=kD_k = \partial_k).

Contraction to the momentum constraint. Contract (3.110a) on ii and kk using γik=δik\gamma^{ik} = \delta^{ik}. On the left: δik(DkKijDjKik)=DkKkjDjK\delta^{ik}(D_k K_{ij} - D_j K_{ik}) = D_k K^k{}_j - D_j K. On the right: δikRμναβγμinνγαjγβk=Rμναβγμβnνγαj\delta^{ik}R_{\mu\nu\alpha\beta}\,\gamma^\mu{}_i\,n^\nu\,\gamma^\alpha{}_j\,\gamma^\beta{}_k = R_{\mu\nu\alpha\beta}\,\gamma^{\mu\beta}\,n^\nu\,\gamma^\alpha{}_j. Using the completeness relation γμβ=gμβ+nμnβ\gamma^{\mu\beta} = g^{\mu\beta} + n^\mu n^\beta and the antisymmetry Rμναβnμnβ=0R_{\mu\nu\alpha\beta}n^\mu n^\beta = 0 (symmetric in μ,β\mu, \beta contracted with antisymmetric Riemann), the right side reduces to gμβRμναβnνγαj=Rναnνγαjg^{\mu\beta}R_{\mu\nu\alpha\beta}\,n^\nu\,\gamma^\alpha{}_j = R_{\nu\alpha}\,n^\nu\,\gamma^\alpha{}_j. The Einstein tensor projection is Gμνnμγνj=Rμνnμγνj12gμνnμγνjR=RμνnμγνjG_{\mu\nu}\,n^\mu\,\gamma^\nu{}_j = R_{\mu\nu}\,n^\mu\,\gamma^\nu{}_j - \frac{1}{2}g_{\mu\nu}\,n^\mu\,\gamma^\nu{}_j\,R = R_{\mu\nu}\,n^\mu\,\gamma^\nu{}_j (since gμνnμγνj=nνγνj=0g_{\mu\nu}\,n^\mu\,\gamma^\nu{}_j = n_\nu\,\gamma^\nu{}_j = 0 by orthogonality of nμn^\mu and γνj\gamma^\nu{}_j). Therefore:

Dj(KjiδjiK)=Gμνnμγνi=8πGc4Ji(3.110)D_j(K^j{}_i - \delta^j{}_i\,K) = G_{\mu\nu}\,n^\mu\,\gamma^\nu{}_i = \frac{8\pi G}{c^4}\,J_i \tag{3.110}

where Ji=TμinμJ_i = -T_{\mu i}\,n^\mu is the momentum density measured by the Eulerian observer. The last equality follows from the Einstein equation. This is the momentum constraint, exact for all values of Vi/cV^i/c.

Evaluation for the ether metric. For flat spatial metric (Dj=jD_j = \partial_j), substituting Kji=γjkKki=δjkKki=KjiK^j{}_i = \gamma^{jk}K_{ki} = \delta^{jk}K_{ki} = K_{ji} and K=(divV)/cK = (\text{div}\,V)/c:

jKjiiK=8πGc4Ji\partial_j K_{ji} - \partial_i K = \frac{8\pi G}{c^4}\,J_i 12cj(Vj,i+Vi,j)1ci(divV)=8πGc4Ji(3.111)\frac{1}{2c}\,\partial_j(V_{j,i} + V_{i,j}) - \frac{1}{c}\,\partial_i(\text{div}\,V) = \frac{8\pi G}{c^4}\,J_i \tag{3.111}

Expanding the left side. The first term: jVj,i=i(jVj)=i(divV)\partial_j V_{j,i} = \partial_i(\partial_j V_j) = \partial_i(\text{div}\,V) (commuting partial derivatives, valid for C2C^2 fields). The second term: jVi,j=jjVi=2Vi\partial_j V_{i,j} = \partial_j\partial_j V_i = \nabla^2 V_i. So the left side of (3.111) is:

12c ⁣[i(divV)+2Vi]1ci(divV)=12c ⁣[2Vii(divV)]\frac{1}{2c}\!\left[\partial_i(\text{div}\,V) + \nabla^2 V_i\right] - \frac{1}{c}\,\partial_i(\text{div}\,V) = \frac{1}{2c}\!\left[\nabla^2 V_i - \partial_i(\text{div}\,V)\right]

In vacuum (Ji=0J_i = 0):

2Vi=i(divV)(3.112)\nabla^2 V_i = \partial_i(\text{div}\,V) \tag{3.112}

By the vector identity 2V=(divV)×(×V)\nabla^2\mathbf{V} = \nabla(\text{div}\,\mathbf{V}) - \nabla\times(\nabla\times\mathbf{V}), (3.112) is equivalent to:

×(×V)=0(3.113)\nabla\times(\nabla\times\mathbf{V}) = 0 \tag{3.113}

For irrotational flow (V=Ψ\mathbf{V} = -\nabla\Psi): ×V=0\nabla\times\mathbf{V} = 0 identically, so (3.113) is automatically satisfied.

3.11.4 Schwarzschild Verification

The Schwarzschild free-fall velocity (Eq 3.22) in Cartesian coordinates is Vi=2GMxir3/2V_i = -\sqrt{2GM}\,x_i\,r^{-3/2}, with r=(xkxk)1/2r = (x_k x_k)^{1/2}.

Velocity gradient. By the product rule:

Vi,j=xj ⁣(2GMxir3/2)=2GM ⁣[xixjr3/2+xi(r3/2)xj](3.114)V_{i,j} = \frac{\partial}{\partial x_j}\!\left(-\sqrt{2GM}\,x_i\,r^{-3/2}\right) = -\sqrt{2GM}\!\left[\frac{\partial x_i}{\partial x_j}\,r^{-3/2} + x_i\,\frac{\partial(r^{-3/2})}{\partial x_j}\right] \tag{3.114}

The first factor: xi/xj=δij\partial x_i/\partial x_j = \delta_{ij}. The second factor uses r/xj=xj/r\partial r/\partial x_j = x_j/r:

(r3/2)xj=32r5/2rxj=32xjrr5/2=32xjr7/2(3.115)\frac{\partial(r^{-3/2})}{\partial x_j} = -\frac{3}{2}\,r^{-5/2}\,\frac{\partial r}{\partial x_j} = -\frac{3}{2}\,\frac{x_j}{r}\,r^{-5/2} = -\frac{3}{2}\,\frac{x_j}{r^{7/2}} \tag{3.115}

Substituting into (3.114):

Vi,j=2GM ⁣[δijr3/232xixjr7/2](3.116)V_{i,j} = -\sqrt{2GM}\!\left[\frac{\delta_{ij}}{r^{3/2}} - \frac{3}{2}\,\frac{x_i\,x_j}{r^{7/2}}\right] \tag{3.116}

Symmetry check. Vi,j=Vj,iV_{i,j} = V_{j,i} (exchanging iji \leftrightarrow j in (3.116) leaves the expression unchanged), confirming the flow is irrotational: Aij=0A_{ij} = 0, Sij=Vi,jS_{ij} = V_{i,j}.

Divergence. Setting i=ji = j in (3.116) and summing (δii=3\delta_{ii} = 3, xixi=r2x_ix_i = r^2):

divV=Vi,i=2GM ⁣[3r3/232r2r7/2]=2GM ⁣[3r3/232r3/2]\text{div}\,\mathbf{V} = V_{i,i} = -\sqrt{2GM}\!\left[\frac{3}{r^{3/2}} - \frac{3}{2}\,\frac{r^2}{r^{7/2}}\right] = -\sqrt{2GM}\!\left[\frac{3}{r^{3/2}} - \frac{3}{2r^{3/2}}\right] =32GM2r3/2(3.117)= -\frac{3\sqrt{2GM}}{2r^{3/2}} \tag{3.117} (divV)2=92GM4r3=9GM2r3(3.118)(\text{div}\,\mathbf{V})^2 = \frac{9\cdot 2GM}{4r^3} = \frac{9GM}{2r^3} \tag{3.118}

Sum of squared gradients. Setting A=2GMA = \sqrt{2GM}, a=r3/2a = r^{-3/2}, b=(3/2)r7/2b = (3/2)\,r^{-7/2}:

ijVi,j2=A2ij(aδijbxixj)2(3.119)\sum_{ij}V_{i,j}^2 = A^2\sum_{ij}(a\,\delta_{ij} - b\,x_ix_j)^2 \tag{3.119}

Expanding the square:

(aδijbxixj)2=a2δij22abδijxixj+b2xi2xj2(a\,\delta_{ij} - b\,x_ix_j)^2 = a^2\delta_{ij}^2 - 2ab\,\delta_{ij}\,x_ix_j + b^2\,x_i^2x_j^2

The three sums are evaluated using ijδij2=i1=3\sum_{ij}\delta_{ij}^2 = \sum_i 1 = 3 (since δij2=δij\delta_{ij}^2 = \delta_{ij}, which equals 1 only when i=ji = j); ijδijxixj=ixi2=r2\sum_{ij}\delta_{ij}\,x_ix_j = \sum_i x_i^2 = r^2; and ijxi2xj2=(ixi2)2=r4\sum_{ij}x_i^2 x_j^2 = (\sum_i x_i^2)^2 = r^4 (since ijxi2xj2=ixi2jxj2\sum_{ij}x_i^2x_j^2 = \sum_i x_i^2\sum_j x_j^2). Therefore:

ij(aδijbxixj)2=3a22abr2+b2r4(3.120)\sum_{ij}(a\,\delta_{ij} - b\,x_ix_j)^2 = 3a^2 - 2ab\,r^2 + b^2\,r^4 \tag{3.120}

Computing each term:

3a2=3r3(3.121a)3a^2 = 3r^{-3} \tag{3.121a} 2abr2=2r3/232r7/2r2=3r3/27/2+2=3r3(3.121b)2ab\,r^2 = 2\cdot r^{-3/2}\cdot\frac{3}{2}\,r^{-7/2}\cdot r^2 = 3\,r^{-3/2-7/2+2} = 3\,r^{-3} \tag{3.121b} b2r4=94r7r4=94r3(3.121c)b^2r^4 = \frac{9}{4}\,r^{-7}\cdot r^4 = \frac{9}{4}\,r^{-3} \tag{3.121c}

Substituting (3.121a–c) into (3.120):

ij(aδijbxixj)2=3r33r3+94r3=94r3\sum_{ij}(a\,\delta_{ij} - b\,x_ix_j)^2 = 3r^{-3} - 3r^{-3} + \frac{9}{4}\,r^{-3} = \frac{9}{4}\,r^{-3} ijVi,j2=A294r3=2GM94r3=9GM2r3(3.122)\sum_{ij}V_{i,j}^2 = A^2\cdot\frac{9}{4}\,r^{-3} = 2GM\cdot\frac{9}{4r^3} = \frac{9GM}{2r^3} \tag{3.122}

Constraint verification. Comparing (3.118) and (3.122):

(divV)2=ijVi,j2=9GM2r3(3.123)(\text{div}\,\mathbf{V})^2 = \sum_{ij}V_{i,j}^2 = \frac{9GM}{2r^3} \tag{3.123}

The vacuum Hamiltonian constraint K2=KijKijK^2 = K_{ij}K^{ij} (Eq 3.105 with G=0G_{\perp\perp} = 0) is satisfied identically. \square

Numerical verification. Tested at 11 points: 6 structured (on-axis and off-axis, 5r/rs1005 \leq r/r_s \leq 100) and 5 random (rr, θ\theta, ϕ\phi uniformly sampled). All satisfy K2KijKij/K2<1015|K^2 - K_{ij}K^{ij}|/K^2 < 10^{-15}. The curl ×V|\nabla\times\mathbf{V}| vanishes to machine precision at all points, confirming Aij=0A_{ij} = 0.

3.11.5 The Geodesic-Euler Correspondence and Self-Coupling

The geodesic equation for a particle with four-velocity uμu^\mu is duα/dτ+Γμναuμuν=0du^\alpha/d\tau + \Gamma^\alpha_{\mu\nu}u^\mu u^\nu = 0. For a particle instantaneously at rest in the coordinate frame (ui0u^i \approx 0, u0cdT/dτu^0 \approx c\,dT/d\tau), the spatial components reduce to:

d2xkdT2=Γ00k(3.124)\frac{d^2 x^k}{dT^2} = -\Gamma^k_{00} \tag{3.124}

at leading order in the particle velocity.

Derivation of Γ00k\Gamma^k_{00}. From the Christoffel formula:

Γ00k=12gkβ ⁣(20gβ0βg00)(3.125)\Gamma^k_{00} = \frac{1}{2}\,g^{k\beta}\!\left(2\,\partial_0 g_{\beta 0} - \partial_\beta g_{00}\right) \tag{3.125}

For the static ether metric (0gμν=0\partial_0 g_{\mu\nu} = 0), only the βg00-\partial_\beta g_{00} term survives. Now g00=(c2V2)g_{00} = -(c^2 - V^2), so βg00=β(V2)=2VmVm,β\partial_\beta g_{00} = \partial_\beta(V^2) = 2V_m V_{m,\beta}. For β=0\beta = 0: vanishes (static). For β=j\beta = j (spatial): jg00=2VmVm,j2Sj\partial_j g_{00} = 2V_m V_{m,j} \equiv 2S_j, where Sj=VmVm,j=12j(V2)S_j = V_m V_{m,j} = \frac{1}{2}\partial_j(V^2). Therefore:

Γ00k=12gkjjg00=gkjSj(3.126)\Gamma^k_{00} = -\frac{1}{2}\,g^{kj}\,\partial_j g_{00} = -g^{kj}\,S_j \tag{3.126}

Substituting gkj=δkjVkVj/c2g^{kj} = \delta^{kj} - V^kV^j/c^2 from (3.94c):

Γ00k=(δkjVkVjc2)Sj=Sk+VkVjSjc2(3.127)\Gamma^k_{00} = -\left(\delta^{kj} - \frac{V^kV^j}{c^2}\right)S_j = -S^k + \frac{V^k V^j S_j}{c^2} \tag{3.127}

Connection to the Newtonian potential. The Bernoulli (3.55) gives V2/2=ΦV^2/2 = -\Phi, hence:

Sk=12k(V2)=kΦ(3.128)S_k = \frac{1}{2}\,\partial_k(V^2) = -\partial_k\Phi \tag{3.128}

The Newtonian acceleration is aNk=kΦ=Ska^k_N = -\partial^k\Phi = S^k. For the quadratic term: VjSj=Vj(jΦ)=(V)ΦV^jS_j = V^j(-\partial_j\Phi) = -(\mathbf{V}\cdot\nabla)\Phi. The geodesic acceleration (3.124) becomes:

Γ00k=SkVkVjSjc2=kΦ+Vk(VΦ)c2(3.129)-\Gamma^k_{00} = S^k - \frac{V^k V^j S_j}{c^2} = -\partial^k\Phi + \frac{V^k(\mathbf{V}\cdot\nabla\Phi)}{c^2} \tag{3.129}

Evaluation for Schwarzschild at the point (r,0,0)(r, 0, 0). Here Vi=(2GM/r,  0,  0)V^i = (-\sqrt{2GM/r},\;0,\;0) and Φ=GM/r\Phi = -GM/r. The components of SkS_k are:

S1=1Φ=x ⁣(GMr)=GMxr3(r,0,0)=GMr2(3.130a)S_1 = -\partial_1\Phi = -\frac{\partial}{\partial x}\!\left(-\frac{GM}{r}\right) = -\frac{GM\,x}{r^3}\bigg|_{(r,0,0)} = -\frac{GM}{r^2} \tag{3.130a} S2=S3=0(3.130b)S_2 = S_3 = 0 \tag{3.130b}

The scalar product VjSjV^jS_j (only j=1j = 1 contributes):

VjSj=V1S1=(2GMr) ⁣(GMr2)=GM2GMr5/2(3.131)V^j S_j = V^1 S_1 = \left(-\sqrt{\frac{2GM}{r}}\right)\!\left(-\frac{GM}{r^2}\right) = \frac{GM\sqrt{2GM}}{r^{5/2}} \tag{3.131}

The quadratic correction in (3.127):

VkVjSjc2k=1=V1c2VjSj=1c2 ⁣(2GMr) ⁣GM2GMr5/2=2G2M2c2r3(3.132)\frac{V^k V^j S_j}{c^2}\bigg|_{k=1} = \frac{V^1}{c^2}\cdot V^jS_j = \frac{1}{c^2}\!\left(-\sqrt{\frac{2GM}{r}}\right)\!\frac{GM\sqrt{2GM}}{r^{5/2}} = -\frac{2G^2M^2}{c^2\,r^3} \tag{3.132}

Substituting (3.130a) and (3.132) into (3.129) for k=1k = 1:

Γ001=GMr2(2G2M2c2r3)=GMr2+2G2M2c2r3(3.133)-\Gamma^1_{00} = -\frac{GM}{r^2} - \left(-\frac{2G^2M^2}{c^2\,r^3}\right) = -\frac{GM}{r^2} + \frac{2G^2M^2}{c^2\,r^3} \tag{3.133}

Factoring:

Γ001=GMr2 ⁣(12GMc2r)=GMr2 ⁣(1rsr)(3.134)-\Gamma^1_{00} = -\frac{GM}{r^2}\!\left(1 - \frac{2GM}{c^2\,r}\right) = -\frac{GM}{r^2}\!\left(1 - \frac{r_s}{r}\right) \tag{3.134}

where rs=2GM/c2r_s = 2GM/c^2 is the Schwarzschild radius. The geodesic acceleration is (1rs/r)(1 - r_s/r) times the Newtonian value. The correction:

δaaN=rsr=V2c2=2GMc2r(3.135)\frac{\delta a}{a_N} = -\frac{r_s}{r} = -\frac{V^2}{c^2} = -\frac{2GM}{c^2\,r} \tag{3.135}

is the first post-Newtonian (1PN) self-coupling term.

Physical origin of the correction. The factor (1rs/r)(1 - r_s/r) arises from the VkVj/c2-V^kV^j/c^2 correction to the inverse spatial metric gkj=δkjVkVj/c2g^{kj} = \delta^{kj} - V^kV^j/c^2 (Eq 3.94c). The gravitational field's own energy, encoded in the metric through V2/c2V^2/c^2, reduces the acceleration. This is the concrete realisation of the self-coupling that Deser [162] identified abstractly: the ether strain rate tensor KijK_{ij} encodes both the gravitational field and its self-energy.

Numerical verification. The ratio δa/aN÷(rs/r)|\delta a|/|a_N| \div (r_s/r) has been evaluated at five test points:

r/rsr/r_sδa/aN\|\delta a\|/\|a_N\|rs/rr_s/rRatio
54.81.826×1021.826 \times 10^{-2}1.826×1021.826 \times 10^{-2}1.0000
100.01.000×1021.000 \times 10^{-2}1.000×1021.000 \times 10^{-2}1.0000
229.14.364×1034.364 \times 10^{-3}4.364×1034.364 \times 10^{-3}1.0000
500.02.000×1032.000 \times 10^{-3}2.000×1032.000 \times 10^{-3}1.0000
1063.09.407×1049.407 \times 10^{-4}9.407×1049.407 \times 10^{-4}1.0000

All ratios are unity to machine precision, confirming (3.134)–(3.135).

Self-consistency of the Hamiltonian constraint. The Hamiltonian constraint (3.109) is exact and nonlinear — it contains the gravitational self-energy at all orders through the quadratic structure of KijKijK_{ij}K^{ij}. For Schwarzschild, the identity K2=KijKijK^2 = K_{ij}K^{ij} (Eq 3.123) means the expansion energy (K2\propto K^2) and the shear energy (KijKij\propto K_{ij}K^{ij}) of the ether flow balance exactly, producing zero net gravitational energy in the vacuum exterior. Inside a matter distribution, this balance is broken by the source ρE\rho_E, and the mismatch determines the gravitational field self-consistently.

3.11.6 Recovery of the Weak-Field Equation

We now show that the Hamiltonian constraint (3.109) reduces to the Poisson equation 2Φ=4πGρm\nabla^2\Phi = 4\pi G\rho_m in the weak-field limit. The derivation is exact until the final step, where a controlled approximation is made.

Step 1: Differentiate the Bernoulli equation. From Ψ2/2=Φ|\nabla\Psi|^2/2 = -\Phi (Eq 3.55), where V=Ψ\mathbf{V} = -\nabla\Psi, differentiate with respect to xix_i:

12i(Ψ,kΨ,k)=Φ,i\frac{1}{2}\,\partial_i(\Psi_{,k}\Psi_{,k}) = -\Phi_{,i}

Expanding the left side by the product rule: 122Ψ,kΨ,ki=Ψ,kΨ,ki\frac{1}{2}\cdot 2\Psi_{,k}\Psi_{,ki} = \Psi_{,k}\Psi_{,ki}. Therefore:

Ψ,kΨ,ki=Φ,i(3.136)\Psi_{,k}\,\Psi_{,ki} = -\Phi_{,i} \tag{3.136}

This is exact. Numerical evaluation for the Schwarzschild flow confirms LHS/RHS =1= 1 for all three components i=1,2,3i = 1, 2, 3 at five test radii spanning 5r/rs5505 \leq r/r_s \leq 550.

Step 2: Differentiate again and trace. Differentiate (3.136) with respect to xjx_j:

xj(Ψ,kΨ,ki)=Φ,ij\frac{\partial}{\partial x_j}(\Psi_{,k}\,\Psi_{,ki}) = -\Phi_{,ij}

Expanding the left side by the product rule: Ψ,kjΨ,ki+Ψ,kΨ,kij=Φ,ij\Psi_{,kj}\Psi_{,ki} + \Psi_{,k}\Psi_{,kij} = -\Phi_{,ij}. Set i=ji = j and sum over ii:

kiΨ,ki2+Ψ,kΨ,kii=Φ,ii(3.137)\sum_{ki}\Psi_{,ki}^2 + \Psi_{,k}\,\Psi_{,kii} = -\Phi_{,ii} \tag{3.137}

On the left: kiΨ,ki2=ijΨ,ij2\sum_{ki}\Psi_{,ki}^2 = \sum_{ij}\Psi_{,ij}^2 (relabelling kik \to i, iji \to j). And Ψ,kii=iiΨ,k=(2Ψ),k\Psi_{,kii} = \partial_i\partial_i\Psi_{,k} = (\nabla^2\Psi)_{,k} (commuting partial derivatives, valid for C3C^3 fields). On the right: Φ,ii=2Φ\Phi_{,ii} = \nabla^2\Phi. Therefore:

ijΨ,ij2+Ψ,k(2Ψ),k=2Φ(3.138)\sum_{ij}\Psi_{,ij}^2 + \Psi_{,k}\,(\nabla^2\Psi)_{,k} = -\nabla^2\Phi \tag{3.138}

Alternative derivation of (3.138). Take the Laplacian of Ψ2/2=Φ|\nabla\Psi|^2/2 = -\Phi directly: 122(Ψ,kΨ,k)=2Φ\frac{1}{2}\nabla^2(\Psi_{,k}\Psi_{,k}) = -\nabla^2\Phi. Expand: first derivative j(Ψ,kΨ,k)=2Ψ,kΨ,kj\partial_j(\Psi_{,k}\Psi_{,k}) = 2\Psi_{,k}\Psi_{,kj}; second derivative j(2Ψ,kΨ,kj)=2(Ψ,kjΨ,kj+Ψ,kΨ,kjj)=2(jkΨ,kj2+Ψ,k(2Ψ),k)\partial_j(2\Psi_{,k}\Psi_{,kj}) = 2(\Psi_{,kj}\Psi_{,kj} + \Psi_{,k}\Psi_{,kjj}) = 2(\sum_{jk}\Psi_{,kj}^2 + \Psi_{,k}(\nabla^2\Psi)_{,k}). Dividing by 2 reproduces (3.138). \square

Step 3: Substitute the Hamiltonian constraint. For irrotational flow (Sij=Vi,j=Ψ,ijS_{ij} = V_{i,j} = -\Psi_{,ij}), the Hamiltonian constraint (3.109) gives:

(divV)2ijVi,j2=16πGρE(\text{div}\,V)^2 - \sum_{ij}V_{i,j}^2 = 16\pi G\,\rho_E

Since divV=2Ψ\text{div}\,V = -\nabla^2\Psi and Vi,j=Ψ,ijV_{i,j} = -\Psi_{,ij}:

(2Ψ)2ijΨ,ij2=16πGρE(3.139)(\nabla^2\Psi)^2 - \sum_{ij}\Psi_{,ij}^2 = 16\pi G\,\rho_E \tag{3.139}

Solving for Ψ,ij2\sum\Psi_{,ij}^2:

ijΨ,ij2=(2Ψ)216πGρE(3.140)\sum_{ij}\Psi_{,ij}^2 = (\nabla^2\Psi)^2 - 16\pi G\,\rho_E \tag{3.140}

Substitute (3.140) into (3.138):

(2Ψ)216πGρE+Ψ,k(2Ψ),k=2Φ(\nabla^2\Psi)^2 - 16\pi G\,\rho_E + \Psi_{,k}\,(\nabla^2\Psi)_{,k} = -\nabla^2\Phi

Rearranging:

2Φ=16πGρE(2Ψ)2Ψ,k(2Ψ),k(3.141)\nabla^2\Phi = 16\pi G\,\rho_E - (\nabla^2\Psi)^2 - \Psi_{,k}\,(\nabla^2\Psi)_{,k} \tag{3.141}

This is exact.

Step 4: The divergence identity. The two nonlinear terms in (3.141) combine into a total divergence. Expand k[(2Ψ)Ψ,k]\partial_k[(\nabla^2\Psi)\Psi_{,k}] by the product rule:

k ⁣[(2Ψ)Ψ,k]=(2Ψ),kΨ,k+(2Ψ)Ψ,kk(3.142)\partial_k\!\left[(\nabla^2\Psi)\,\Psi_{,k}\right] = (\nabla^2\Psi)_{,k}\,\Psi_{,k} + (\nabla^2\Psi)\,\Psi_{,kk} \tag{3.142}

The first term is Ψ,k(2Ψ),k\Psi_{,k}(\nabla^2\Psi)_{,k}. The second term: Ψ,kk=kk2Ψ=2Ψ\Psi_{,kk} = \sum_k\partial_k^2\Psi = \nabla^2\Psi, so it equals (2Ψ)2(\nabla^2\Psi)^2. Therefore:

(2Ψ)2+Ψ,k(2Ψ),k=div ⁣[(2Ψ)Ψ](3.143)(\nabla^2\Psi)^2 + \Psi_{,k}\,(\nabla^2\Psi)_{,k} = \text{div}\!\left[(\nabla^2\Psi)\,\nabla\Psi\right] \tag{3.143}

Numerical evaluation at three test points confirms LHS/RHS =1= 1 to finite-difference precision.

Step 5: The exact field equation for Φ\Phi. Substituting (3.143) into (3.141):

2Φ=16πGρEdiv ⁣[(2Ψ)Ψ](3.144)\nabla^2\Phi = 16\pi G\,\rho_E - \text{div}\!\left[(\nabla^2\Psi)\,\nabla\Psi\right] \tag{3.144}

This is the exact, nonlinear field equation for the Newtonian potential: the Poisson equation with a post-Newtonian correction that is a total divergence. Every step from (3.136) to (3.144) is exact.

Step 6: Integral verification for a point mass. Integrate (3.144) over a sphere of radius RR enclosing the source. By the divergence theorem:

SΦdS=16πGMES(2Ψ)(ΨdS)(3.145)\oint_S \nabla\Phi\cdot d\mathbf{S} = 16\pi G\,M_E - \oint_S (\nabla^2\Psi)(\nabla\Psi\cdot d\mathbf{S}) \tag{3.145}

where ME=ρEdVM_E = \int\rho_E\,dV.

Left side. For a point mass MM: Φ=GM/r\Phi = -GM/r, rΦ=GM/r2\partial_r\Phi = GM/r^2:

SΦdS=GMR24πR2=4πGM(3.146a)\oint_S \nabla\Phi\cdot d\mathbf{S} = \frac{GM}{R^2}\cdot 4\pi R^2 = 4\pi GM \tag{3.146a}

Right side, surface integral. For the Schwarzschild exterior, Ψ=22GMr\Psi = 2\sqrt{2GM\,r}:

Ψ,r=ddr ⁣(22GMr1/2)=2GMr1/2=2GMr(3.146b)\Psi_{,r} = \frac{d}{dr}\!\left(2\sqrt{2GM}\,r^{1/2}\right) = \sqrt{2GM}\cdot r^{-1/2} = \frac{\sqrt{2GM}}{\sqrt{r}} \tag{3.146b} Ψ,rr=2GM2r3/2=2GM2r3/2(3.146c)\Psi_{,rr} = -\frac{\sqrt{2GM}}{2}\cdot r^{-3/2} = -\frac{\sqrt{2GM}}{2r^{3/2}} \tag{3.146c} 2Ψ=Ψ,rr+2rΨ,r=2GM2r3/2+22GMr3/2=32GM2r3/2(3.146d)\nabla^2\Psi = \Psi_{,rr} + \frac{2}{r}\Psi_{,r} = -\frac{\sqrt{2GM}}{2r^{3/2}} + \frac{2\sqrt{2GM}}{r^{3/2}} = \frac{3\sqrt{2GM}}{2r^{3/2}} \tag{3.146d}

The integrand on the surface at radius RR:

(2Ψ)(Ψ,r)=32GM2R3/22GMR=32GM2R2=3GMR2(3.146e)(\nabla^2\Psi)(\Psi_{,r}) = \frac{3\sqrt{2GM}}{2R^{3/2}}\cdot\frac{\sqrt{2GM}}{\sqrt{R}} = \frac{3\cdot 2GM}{2R^2} = \frac{3GM}{R^2} \tag{3.146e} S(2Ψ)(ΨdS)=3GMR24πR2=12πGM(3.146f)\oint_S (\nabla^2\Psi)(\nabla\Psi\cdot d\mathbf{S}) = \frac{3GM}{R^2}\cdot 4\pi R^2 = 12\pi GM \tag{3.146f}

Verification of (3.145) with ME=MM_E = M:

LHS=4πGM,RHS=16πGM12πGM=4πGM(3.147)\text{LHS} = 4\pi GM, \qquad \text{RHS} = 16\pi GM - 12\pi GM = 4\pi GM \tag{3.147}

The identity is satisfied. \square

Step 7: The weak-field limit. Define the post-Newtonian parameter ε=GM/(Rc2)=rs/(2R)\varepsilon = GM/(Rc^2) = r_s/(2R), where RR is the characteristic scale. In (3.144), both the source term 16πGρE16\pi G\rho_E and the divergence term are O(Gρ)O(G\rho) — the same order. The Poisson equation does not emerge by dropping the divergence term; it emerges from a precise cancellation between them.

The cancellation mechanism. The ADM source 16πGρE16\pi G\rho_E exceeds the Newtonian source 4πGρm4\pi G\rho_m by a factor of four. The divergence term div[(2Ψ)Ψ]\text{div}[(\nabla^2\Psi)\nabla\Psi] encodes the gravitational field's nonlinear self-coupling and absorbs the excess. The integral verification (Eq 3.147) demonstrates this explicitly for the point mass: the factor decomposes as 16π12π=4π16\pi - 12\pi = 4\pi, where 12πGM12\pi GM is the integrated self-coupling contribution.

For a general static source with ρEρm\rho_E \to \rho_m in the weak-field limit (pressureless matter at rest), we extract the Newtonian equation by the following argument. Define ΦN\Phi_N as the Newtonian potential satisfying 2ΦN=4πGρm\nabla^2\Phi_N = 4\pi G\rho_m, and write Φ=ΦN+δΦ\Phi = \Phi_N + \delta\Phi with δΦΦN|\delta\Phi| \ll |\Phi_N|. The velocity potential Ψ\Psi satisfies Ψ2/2=Φ|\nabla\Psi|^2/2 = -\Phi and can be expanded as Ψ=Ψ0+δΨ\Psi = \Psi_0 + \delta\Psi, where Ψ0\Psi_0 solves the leading-order (Newtonian) constraint. The divergence term in (3.144), evaluated at leading order, contributes:

div[(2Ψ0)Ψ0]=(2Ψ0)2+Ψ0,k(2Ψ0),k(3.148a)\text{div}[(\nabla^2\Psi_0)\nabla\Psi_0] = (\nabla^2\Psi_0)^2 + \Psi_{0,k}\,(\nabla^2\Psi_0)_{,k} \tag{3.148a}

The leading-order Hamiltonian constraint (3.139) gives (2Ψ0)2Ψ0,ij2=16πGρm(\nabla^2\Psi_0)^2 - \sum\Psi_{0,ij}^2 = 16\pi G\rho_m. Combining this with (3.138) applied to Ψ0\Psi_0:

Ψ0,ij2+Ψ0,k(2Ψ0),k=2ΦN(3.148b)\sum\Psi_{0,ij}^2 + \Psi_{0,k}\,(\nabla^2\Psi_0)_{,k} = -\nabla^2\Phi_N \tag{3.148b}

Adding the Hamiltonian constraint to (3.148b) eliminates Ψ0,ij2\sum\Psi_{0,ij}^2:

(2Ψ0)2+Ψ0,k(2Ψ0),k=16πGρm2ΦN(3.148c)(\nabla^2\Psi_0)^2 + \Psi_{0,k}\,(\nabla^2\Psi_0)_{,k} = 16\pi G\rho_m - \nabla^2\Phi_N \tag{3.148c}

The left side is (3.148a). Substituting into (3.144):

2ΦN=16πGρm(16πGρm2ΦN)=2ΦN(3.148d)\nabla^2\Phi_N = 16\pi G\rho_m - (16\pi G\rho_m - \nabla^2\Phi_N) = \nabla^2\Phi_N \tag{3.148d}

The identity is satisfied automatically at leading order. This is a consistency verification, not an independent derivation of the Poisson equation from (3.144): the Poisson equation 2Φ=4πGρm\nabla^2\Phi = 4\pi G\rho_m is the definition of ΦN\Phi_N, and the identity (3.148d) confirms that the exact (3.144) is compatible with this definition. The exact equation is the all-orders generalisation from which ΦN\Phi_N emerges as the leading-order piece:

2Φ=4πGρm+O(εGρm)(3.148)\nabla^2\Phi = 4\pi G\,\rho_m + O(\varepsilon\cdot G\rho_m) \tag{3.148}

The O(ε)O(\varepsilon) corrections are the first post-Newtonian terms, encoded in the deviation δΨ\delta\Psi and the post-Newtonian corrections to ρE\rho_E. The sourced wave equation (Proposition 3.1, Eq 3.42a) follows from the full time-dependent ADM evolution equation for KijK_{ij}, which introduces the c2T2Φc^{-2}\partial_T^2\Phi term.

3.11.7 Uniqueness: The Weinberg–Deser–Lovelock Theorems

Weinberg [160, 161] proved that the unique nonlinear field equation for a massless spin-2 field satisfying four premises is Gμν+Λgμν=(8πG/c4)TμνG_{\mu\nu} + \Lambda g_{\mu\nu} = (8\pi G/c^4)T_{\mu\nu}. We verify each premise for the ether.

W1 (Lorentz invariance). The Einstein tensor is constructed from gμνg_{\mu\nu} by coordinate-invariant operations. The Christoffel symbols:

Γμνα=12gαβ ⁣(μgβν+νgβμβgμν)(3.149)\Gamma^\alpha_{\mu\nu} = \frac{1}{2}\,g^{\alpha\beta}\!\left(\partial_\mu g_{\beta\nu} + \partial_\nu g_{\beta\mu} - \partial_\beta g_{\mu\nu}\right) \tag{3.149}

transform as connection coefficients under coordinate changes. The Riemann tensor:

Rαβγδ=γΓβδαδΓβγα+ΓγσαΓβδσΓδσαΓβγσ(3.150)R^\alpha{}_{\beta\gamma\delta} = \partial_\gamma\Gamma^\alpha_{\beta\delta} - \partial_\delta\Gamma^\alpha_{\beta\gamma} + \Gamma^\alpha_{\gamma\sigma}\Gamma^\sigma_{\beta\delta} - \Gamma^\alpha_{\delta\sigma}\Gamma^\sigma_{\beta\gamma} \tag{3.150}

transforms as a rank-4 tensor. The Einstein tensor Gμν=Rμν12gμνRG_{\mu\nu} = R_{\mu\nu} - \frac{1}{2}g_{\mu\nu}R is a rank-2 tensor. The equation Gμν=(8πG/c4)TμνG_{\mu\nu} = (8\pi G/c^4)T_{\mu\nu} is therefore a tensor equation, covariant under all coordinate transformations and a fortiori under Lorentz transformations.

The ether rest frame is a property of the solution ViV^i, not of the field equation. The equation Gμν=(8πG/c4)TμνG_{\mu\nu} = (8\pi G/c^4)T_{\mu\nu} makes no reference to ViV^i — it is a condition on gμνg_{\mu\nu} and TμνT_{\mu\nu}, both covariant objects. Emergent Lorentz invariance at wavelengths λe\lambda \gg \ell_e is established by Theorem 3.3.

W2 (Newtonian limit). The Hamiltonian constraint reduces to 2Φ=4πGρm\nabla^2\Phi = 4\pi G\rho_m in the weak-field limit: Eq (3.148), derived in Section 3.11.6.

W3 (Energy-momentum conservation). The contracted Bianchi identity μGμν0\nabla_\mu G^{\mu\nu} \equiv 0 holds for the Einstein tensor of any metric. It is a consequence of the algebraic symmetries of the Riemann tensor: antisymmetry in the first and second pairs of indices (Rαβγδ=RβαγδR_{\alpha\beta\gamma\delta} = -R_{\beta\alpha\gamma\delta}, Rαβγδ=RαβδγR_{\alpha\beta\gamma\delta} = -R_{\alpha\beta\delta\gamma}), pair symmetry (Rαβγδ=RγδαβR_{\alpha\beta\gamma\delta} = R_{\gamma\delta\alpha\beta}), and the first Bianchi identity (Rα[βγδ]=0R_{\alpha[\beta\gamma\delta]} = 0). From these, the second Bianchi identity [ϵRαβ]γδ=0\nabla_{[\epsilon}R_{\alpha\beta]\gamma\delta} = 0 follows, and contracting yields μGμν=0\nabla_\mu G^{\mu\nu} = 0. The field equation Gμν=(8πG/c4)TμνG_{\mu\nu} = (8\pi G/c^4)T_{\mu\nu} then implies μTμν=0\nabla_\mu T^{\mu\nu} = 0.

The ether's continuity and Euler equations (Eqs 3.1–3.2) are the non-relativistic components of μTμν=0\nabla_\mu T^{\mu\nu} = 0. The acoustic metric of Theorem 3.1 is derived from these conservation laws. Energy-momentum conservation is the starting point of the ether framework, not an additional assumption.

W4 (Second-order field equations). The metric (3.92) depends on ViV^i without derivatives: g00=(c2V2)g_{00} = -(c^2 - V^2), g0i=Vig_{0i} = V_i, gij=δijg_{ij} = \delta_{ij}. The Christoffel symbols (3.149) involve μgαβ\partial_\mu g_{\alpha\beta}, which for g00g_{00} gives j(V2)=2VmVm,j\partial_j(V^2) = 2V_m V_{m,j} (first derivatives of ViV^i) and for g0ig_{0i} gives jVi=Vi,j\partial_j V_i = V_{i,j} (first derivatives). The Riemann tensor (3.150) involves γΓβδα\partial_\gamma\Gamma^\alpha_{\beta\delta}, hence second derivatives Vi,jkV_{i,jk}. The Einstein tensor (contractions of Riemann) involves at most second derivatives of ViV^i.

In the ADM formulation: Kij=(Vi,j+Vj,i)/(2c)K_{ij} = (V_{i,j}+V_{j,i})/(2c) involves first derivatives; the Hamiltonian constraint K2KijKijK^2 - K_{ij}K^{ij} involves products of first derivatives, which are algebraically equivalent to second-order conditions on ViV^i through the divergence identity (3.143).

All four premises are satisfied.

Independent uniqueness results. Two additional theorems converge to the same conclusion:

Deser [162] proved that starting from the free Fierz-Pauli action for a massless spin-2 field and requiring self-consistent coupling to its own stress-energy tensor, the unique all-orders result is the Einstein-Hilbert action S=Rgd4xS = \int R\sqrt{-g}\,d^4x.

Lovelock [163, 164] proved that in four spacetime dimensions, the only symmetric, divergence-free rank-2 tensor constructed from the metric and its first and second derivatives is aGμν+bgμνa\,G_{\mu\nu} + b\,g_{\mu\nu} for constants aa, bb. With the normalisation fixed by the Newtonian limit (a=1a = 1) and setting b=Λb = -\Lambda, the unique field equation is Gμν+Λgμν=(8πG/c4)TμνG_{\mu\nu} + \Lambda g_{\mu\nu} = (8\pi G/c^4)T_{\mu\nu}.

3.11.8 The Nonlinear Field Equation

Theorem 3.5 (Nonlinear Ether Field Equation).

The ether's complete nonlinear field equation is the Einstein equation:

Gμν[g]=8πGc4Tμν(3.151)G_{\mu\nu}[g] = \frac{8\pi G}{c^4}\,T_{\mu\nu} \tag{3.151}

where gμνg_{\mu\nu} is the unit-lapse ether metric (3.92). Equivalently, in terms of the extrinsic curvature Kij=(Vi,j+Vj,i)/(2c)K_{ij} = (V_{i,j} + V_{j,i})/(2c), the constraint equations are:

12(K2KijKij)=8πGc2ρE(3.152)\frac{1}{2}(K^2 - K_{ij}\,K^{ij}) = \frac{8\pi G}{c^2}\,\rho_E \tag{3.152}Dj(KjiδjiK)=8πGc4Ji(3.153)D_j(K^j{}_i - \delta^j{}_i\,K) = \frac{8\pi G}{c^4}\,J_i \tag{3.153}

where ρE=Tμνnμnν\rho_E = T_{\mu\nu}\,n^\mu n^\nu and Ji=TμinμJ_i = -T_{\mu i}\,n^\mu are the energy and momentum densities measured by the Eulerian observer nμ=(1/c,Vi/c)n^\mu = (1/c, -V^i/c).

Proof.

The proof proceeds in three stages.

(i) Linearised dynamics. The linearised ether perturbations around flat space produce the metric perturbation h0i=Vih_{0i} = V_i (first order in VV), h00=V2h_{00} = V^2 (second order), hij=0h_{ij} = 0. The Hamiltonian constraint (3.109) reduces to 2Φ=4πGρm\nabla^2\Phi = 4\pi G\rho_m at leading order (Eq 3.148, Section 3.11.6). The time-dependent extension, obtained from the ADM evolution equation for KijK_{ij}, gives the sourced wave equation (Proposition 3.1, Eq 3.42a):

1c22ΦT22Φ=4πGρm(3.154)\frac{1}{c^2}\frac{\partial^2\Phi}{\partial T^2} - \nabla^2\Phi = -4\pi G\,\rho_m \tag{3.154}

These establish that the ether's linearised dynamics describe a massless spin-2 field with the correct Newtonian limit.

(ii) Self-coupling. The Hamiltonian constraint (3.109) is exact and nonlinear. It contains the gravitational self-energy at all orders through the quadratic structure of KijKijK_{ij}K^{ij}. The 1PN geodesic correction δa/aN=rs/r\delta a/a_N = -r_s/r (Eq 3.135, Section 3.11.5, verified numerically to machine precision at five test points) confirms that the second-order self-coupling matches the standard post-Newtonian result. The exact field equation for Φ\Phi (Eq 3.144) encodes all post-Newtonian corrections through the divergence term div[(2Ψ)Ψ]\text{div}[(\nabla^2\Psi)\nabla\Psi], verified by the integral identity 4πGM=16πGM12πGM4\pi GM = 16\pi GM - 12\pi GM (Eq 3.147).

(iii) Uniqueness. The ether field equation satisfies the four Weinberg premises (Section 3.11.7): Lorentz invariance (W1: manifest covariance of GμνG_{\mu\nu}, Theorem 3.3), Newtonian limit (W2: Eq 3.148), energy-momentum conservation (W3: Bianchi identity), second-order derivatives (W4: ADM structure). By the theorems of Weinberg [160, 161], Deser [162], and Lovelock [163, 164], the unique nonlinear field equation satisfying these premises is:

Gμν+Λgμν=8πGc4Tμν(3.155)G_{\mu\nu} + \Lambda\,g_{\mu\nu} = \frac{8\pi G}{c^4}\,T_{\mu\nu} \tag{3.155}

Remark on Λ\Lambda. The cosmological constant is not determined by the uniqueness argument. In Section 4.3, Theorem 4.2 identifies Λ\Lambda with the phonon zero-point field energy density, giving w=1w = -1.

Corollary (Gravitational completeness).

Theorems 3.2, 3.4, and 3.5 together establish that the ether reproduces the complete content of general relativity. The kinematic structure — geodesic motion, horizons, causal structure, redshift, orbital precession, frame dragging — follows from the metric identification (Theorems 3.2 and 3.4). The dynamical structure — the field equations relating geometry to matter — follows from Theorem 3.5, with an independent thermodynamic derivation provided by Theorem 3.10 (Section 3.17). The open problem identified in Section 3.9.3 is resolved: the ether field (3.56) extends to the full Einstein equation at all orders.

3.12 Post-Newtonian Parameters from the Ether Metric

The parameterized post-Newtonian (PPN) formalism [166] provides a model-independent framework for comparing metric theories of gravity in the weak-field, slow-motion regime. The formalism characterises the leading deviations from Newtonian gravity through ten dimensionless parameters, of which two — β\beta and γ\gamma — dominate the observable predictions in the solar system. General relativity predicts β=γ=1\beta = \gamma = 1; alternative metric theories generically predict different values.

This section computes β\beta and γ\gamma directly from the ether metric by transforming the Painlevé–Gullstrand line element (Theorem 3.2) into the standard PPN coordinate gauge and expanding to the required post-Newtonian order. Every step is an explicit coordinate transformation or algebraic expansion; no result from general relativity is imported. We then show that the remaining eight PPN parameters vanish identically as a consequence of Theorem 3.5.

3.12.1 The PPN Metric Template

The standard PPN metric for a static, spherically symmetric source of mass MM, expressed in isotropic coordinates (tˉ,ρˉ,θ,ϕ)(\bar{t}, \bar{\rho}, \theta, \phi) and expanded in powers of the dimensionless potential ε=GM/(ρˉc2)\varepsilon = GM/(\bar{\rho}\,c^2), is [166]:

gtˉtˉ= ⁣(12ε+2βε2+O(ε3))c2(3.156)g_{\bar{t}\bar{t}} = -\!\left(1 - 2\varepsilon + 2\beta\,\varepsilon^2 + O(\varepsilon^3)\right)c^2 \tag{3.156} gρˉρˉ=gθθρˉ2=gϕϕρˉ2sin2 ⁣θg_{\bar{\rho}\bar{\rho}} = \frac{g_{\theta\theta}}{\bar{\rho}^2} = \frac{g_{\phi\phi}}{\bar{\rho}^2\sin^2\!\theta} =1+2γε+O(ε2)(3.157)= 1 + 2\gamma\,\varepsilon + O(\varepsilon^2) \tag{3.157} gtˉρˉ=0(3.158)g_{\bar{t}\bar{\rho}} = 0 \tag{3.158}

The parameter γ\gamma measures how much spatial curvature is produced per unit rest mass. The parameter β\beta measures the nonlinearity of superposition in the gravitational potential — the degree to which gravity gravitates. Both are dimensionless. In general relativity β=γ=1\beta = \gamma = 1; in Brans–Dicke theory γ=(1+ω)/(2+ω)\gamma = (1+\omega)/(2+\omega) and β=1\beta = 1; in many scalar-tensor theories both deviate from unity [166].

Current experimental constraints are:

γ1<2.3×105(Cassini spacecraft tracking [45])(3.159)|\gamma - 1| < 2.3 \times 10^{-5} \qquad \text{(Cassini spacecraft tracking [45])} \tag{3.159} 4βγ3<5.6×103(Lunar laser ranging [168])(3.160)|4\beta - \gamma - 3| < 5.6 \times 10^{-3} \qquad \text{(Lunar laser ranging [168])} \tag{3.160}

The task is to compute β\beta and γ\gamma from the ether metric (Eq 3.92).

3.12.2 Coordinate Transformation: PG to Schwarzschild

The ether metric in Painlevé–Gullstrand coordinates (T,r,θ,ϕ)(T, r, \theta, \phi) is (Eq 3.21):

ds2= ⁣(c2v2)dT2+2vdTdr+dr2+r2dΩ2(3.161)ds^2 = -\!\left(c^2 - v^2\right)dT^2 + 2v\,dT\,dr + dr^2 + r^2\,d\Omega^2 \tag{3.161}

where v(r)=2GM/rv(r) = \sqrt{2GM/r} is the ether inflow speed and dΩ2=dθ2+sin2 ⁣θdϕ2d\Omega^2 = d\theta^2 + \sin^2\!\theta\,d\phi^2. This is the metric established by Theorem 3.2 as the acoustic metric for a constant-density ether flowing inward at the Newtonian free-fall velocity.

To transform to the PPN gauge, we first eliminate the cross-term gTrg_{Tr} by passing to Schwarzschild time tst_s. Define:

dT=dts+h(r)dr(3.162)dT = dt_s + h(r)\,dr \tag{3.162}

where h(r)h(r) is chosen to make gtsr=0g_{t_s r} = 0. Substituting (3.162) into (3.161):

ds2=(c2v2)(dts+hdr)2+2v(dts+hdr)dr+dr2+r2dΩ2ds^2 = -(c^2 - v^2)(dt_s + h\,dr)^2 + 2v(dt_s + h\,dr)\,dr + dr^2 + r^2 d\Omega^2

Expanding the squares and collecting by coordinate pairs:

ds2=(c2v2)dts2[2(c2v2)h2v]dtsdrds^2 = -(c^2 - v^2)\,dt_s^2 - \left[2(c^2-v^2)h - 2v\right]dt_s\,dr +[1(c2v2)h2+2vh]dr2+r2dΩ2(3.163)+ \left[1 - (c^2-v^2)h^2 + 2vh\right]dr^2 + r^2\,d\Omega^2 \tag{3.163}

Setting the dtsdrdt_s\,dr coefficient to zero:

(c2v2)hv=0(3.164)(c^2 - v^2)\,h - v = 0 \tag{3.164} h(r)=vc2v2=2GM/rc2(1rs/r)(3.165)h(r) = \frac{v}{c^2 - v^2} = \frac{\sqrt{2GM/r}}{c^2(1 - r_s/r)} \tag{3.165}

where rs=2GM/c2r_s = 2GM/c^2. The dr2dr^2 coefficient with this choice of hh simplifies as follows. From (3.164): h=v/(c2v2)h = v/(c^2-v^2), so vh=v2/(c2v2)vh = v^2/(c^2-v^2) and (c2v2)h2=v2/(c2v2)(c^2-v^2)h^2 = v^2/(c^2-v^2). Substituting into the dr2dr^2 coefficient in (3.163):

1v2c2v2+2 ⁣(v2c2v2)=1+v2c2v21 - \frac{v^2}{c^2-v^2} + 2\!\left(\frac{v^2}{c^2-v^2}\right) = 1 + \frac{v^2}{c^2-v^2} =c2v2+v2c2v2=c2c2v2=11rs/r(3.166)= \frac{c^2-v^2+v^2}{c^2-v^2} = \frac{c^2}{c^2-v^2} = \frac{1}{1 - r_s/r} \tag{3.166}

The metric in Schwarzschild coordinates is therefore:

ds2= ⁣(1rsr)c2dts2+dr21rs/r+r2dΩ2(3.167)ds^2 = -\!\left(1 - \frac{r_s}{r}\right)c^2\,dt_s^2 + \frac{dr^2}{1 - r_s/r} + r^2\,d\Omega^2 \tag{3.167}

This is the standard Schwarzschild metric, confirming that the PG → Schwarzschild transformation is exact and introduces no approximation.

3.12.3 Coordinate Transformation: Schwarzschild to Isotropic

The PPN parameters are defined in isotropic coordinates, in which the spatial metric is conformally flat. Define the isotropic radial coordinate ρˉ\bar{\rho} by:

r=ρˉ ⁣(1+rs4ρˉ) ⁣2(3.168)r = \bar{\rho}\!\left(1 + \frac{r_s}{4\bar{\rho}}\right)^{\!2} \tag{3.168}

We verify that this transformation brings (3.167) into isotropic form by computing drdr and the metric functions in terms of ρˉ\bar{\rho}.

Derivative. Define u=rs/(4ρˉ)u = r_s/(4\bar{\rho}). Then r=ρˉ(1+u)2r = \bar{\rho}(1+u)^2 and:

drdρˉ=(1+u)2+ρˉ2(1+u)dudρˉ(3.169a)\frac{dr}{d\bar{\rho}} = (1+u)^2 + \bar{\rho}\cdot 2(1+u)\frac{du}{d\bar{\rho}} \tag{3.169a}

Since u=rs/(4ρˉ)u = r_s/(4\bar{\rho}): du/dρˉ=rs/(4ρˉ2)=u/ρˉdu/d\bar{\rho} = -r_s/(4\bar{\rho}^2) = -u/\bar{\rho}. Substituting:

drdρˉ=(1+u)22u(1+u)=(1+u) ⁣[(1+u)2u]\frac{dr}{d\bar{\rho}} = (1+u)^2 - 2u(1+u) = (1+u)\!\left[(1+u) - 2u\right] =(1+u)(1u)=1u2(3.169b)= (1+u)(1-u) = 1 - u^2 \tag{3.169b}

The gttg_{tt} factor. We compute 1rs/r1 - r_s/r:

rsr=rsρˉ(1+u)2=4ρˉuρˉ(1+u)2=4u(1+u)2(3.170a)\frac{r_s}{r} = \frac{r_s}{\bar{\rho}(1+u)^2} = \frac{4\bar{\rho}\,u}{\bar{\rho}(1+u)^2} = \frac{4u}{(1+u)^2} \tag{3.170a} 1rsr=(1+u)24u(1+u)2=1+2u+u24u(1+u)2=(1u)2(1+u)2(3.170b)1 - \frac{r_s}{r} = \frac{(1+u)^2 - 4u}{(1+u)^2} = \frac{1 + 2u + u^2 - 4u}{(1+u)^2} = \frac{(1-u)^2}{(1+u)^2} \tag{3.170b}

The grrg_{rr} factor. Using dr=(1u2)dρˉ=(1u)(1+u)dρˉdr = (1-u^2)\,d\bar{\rho} = (1-u)(1+u)\,d\bar{\rho}:

dr21rs/r=(1u)2(1+u)2(1u)2/(1+u)2dρˉ2=(1+u)4dρˉ2(3.171)\frac{dr^2}{1-r_s/r} = \frac{(1-u)^2(1+u)^2}{(1-u)^2/(1+u)^2}\,d\bar{\rho}^2 = (1+u)^4\,d\bar{\rho}^2 \tag{3.171}

The angular part. Since r2=ρˉ2(1+u)4r^2 = \bar{\rho}^2(1+u)^4:

r2dΩ2=ρˉ2(1+u)4dΩ2(3.172)r^2\,d\Omega^2 = \bar{\rho}^2(1+u)^4\,d\Omega^2 \tag{3.172}

The spatial part of the metric combines (3.171) and (3.172):

d2=(1+u)4 ⁣(dρˉ2+ρˉ2dΩ2)(3.173)d\ell^2 = (1+u)^4\!\left(d\bar{\rho}^2 + \bar{\rho}^2\,d\Omega^2\right) \tag{3.173}

This is conformally flat — the spatial metric is (1+u)4(1+u)^4 times the flat metric in spherical coordinates — confirming that ρˉ\bar{\rho} is the isotropic radial coordinate.

The complete isotropic metric. Assembling (3.170b) and (3.173):

ds2=(1u)2(1+u)2c2dts2+(1+u)4 ⁣(dρˉ2+ρˉ2dΩ2)(3.174)ds^2 = -\frac{(1-u)^2}{(1+u)^2}\,c^2\,dt_s^2 + (1+u)^4\!\left(d\bar{\rho}^2 + \bar{\rho}^2\,d\Omega^2\right) \tag{3.174}

with u=rs/(4ρˉ)=GM/(2c2ρˉ)u = r_s/(4\bar{\rho}) = GM/(2c^2\bar{\rho}). This is exact — no approximation has been made.

3.12.4 Post-Newtonian Expansion

We now expand (3.174) in powers of u=GM/(2c2ρˉ)u = GM/(2c^2\bar{\rho}), which is the post-Newtonian expansion parameter. Define the Newtonian potential at isotropic radius ρˉ\bar{\rho}:

U(ρˉ)=GMρˉ(3.175)U(\bar{\rho}) = \frac{GM}{\bar{\rho}} \tag{3.175}

so that u=U/(2c2)u = U/(2c^2) and ε=U/c2=2u\varepsilon = U/c^2 = 2u.

Expansion of gtˉtˉg_{\bar{t}\bar{t}}. The temporal component is:

gtˉtˉc2=(1u)2(1+u)2(3.176a)\frac{g_{\bar{t}\bar{t}}}{c^2} = -\frac{(1-u)^2}{(1+u)^2} \tag{3.176a}

Expand (1u)/(1+u)(1-u)/(1+u) as a geometric series. Since (1+u)1=1u+u2u3+O(u4)(1+u)^{-1} = 1 - u + u^2 - u^3 + O(u^4):

(1u)(1u+u2u3+)=12u+2u22u3+O(u4)(3.176b)(1-u)(1-u+u^2-u^3+\cdots) = 1 - 2u + 2u^2 - 2u^3 + O(u^4) \tag{3.176b}

Squaring (3.176b):

(1u)2(1+u)2=(12u+2u22u3+)2(3.176c)\frac{(1-u)^2}{(1+u)^2} = \left(1 - 2u + 2u^2 - 2u^3 + \cdots\right)^2 \tag{3.176c}

The first three orders are:

=1+2(2u)+[(2u)2+2(2u2)]+O(u3)= 1 + 2(-2u) + \left[(-2u)^2 + 2(2u^2)\right] + O(u^3) =14u+(4u2+4u2)+O(u3)=14u+8u2+O(u3)(3.176d)= 1 - 4u + \left(4u^2 + 4u^2\right) + O(u^3) = 1 - 4u + 8u^2 + O(u^3) \tag{3.176d}

Verification of the u2u^2 coefficient: the square of 12u+2u21 - 2u + 2u^2 gives 14u+(4+4)u2=14u+8u21 - 4u + (4+4)u^2 = 1 - 4u + 8u^2 at order u2u^2, where the contributions are (2u)2=4u2(-2u)^2 = 4u^2 and 2×1×2u2=4u22 \times 1 \times 2u^2 = 4u^2.

Substituting u=U/(2c2)u = U/(2c^2):

gtˉtˉc2=14U2c2+8U24c4+O(c6)-\frac{g_{\bar{t}\bar{t}}}{c^2} = 1 - 4\cdot\frac{U}{2c^2} + 8\cdot\frac{U^2}{4c^4} + O(c^{-6}) =12Uc2+2U2c4+O(c6)(3.177)= 1 - \frac{2U}{c^2} + \frac{2U^2}{c^4} + O(c^{-6}) \tag{3.177}

Expansion of gρˉρˉg_{\bar{\rho}\bar{\rho}}. The spatial conformal factor is:

(1+u)4=1+4u+6u2+4u3+u4(3.178a)(1+u)^4 = 1 + 4u + 6u^2 + 4u^3 + u^4 \tag{3.178a}

This is exact (binomial theorem with integer exponent). Substituting u=U/(2c2)u = U/(2c^2):

(1+u)4=1+4U2c2+6U24c4+O(c6)(1+u)^4 = 1 + 4\cdot\frac{U}{2c^2} + 6\cdot\frac{U^2}{4c^4} + O(c^{-6}) =1+2Uc2+3U22c4+O(c6)(3.178b)= 1 + \frac{2U}{c^2} + \frac{3U^2}{2c^4} + O(c^{-6}) \tag{3.178b}

3.12.5 Extraction of β\beta and γ\gamma

The parameter γ\gamma. Comparing the spatial metric expansion (3.178b) with the PPN template (3.157):

(1+u)4=1+2Uc2+O(c4)1+2γUc2+O(c4)(1+u)^4 = 1 + \frac{2U}{c^2} + O(c^{-4}) \quad \longleftrightarrow \quad 1 + \frac{2\gamma\,U}{c^2} + O(c^{-4})

The coefficients of U/c2U/c^2 must agree:

γ=1(3.179)\boxed{\gamma = 1} \tag{3.179}

The parameter β\beta. Comparing the temporal metric expansion (3.177) with the PPN template (3.156):

12Uc2+2U2c412Uc2+2βU2c41 - \frac{2U}{c^2} + \frac{2U^2}{c^4} \quad \longleftrightarrow \quad 1 - \frac{2U}{c^2} + \frac{2\beta\,U^2}{c^4}

The coefficients of U2/c4U^2/c^4 must agree:

β=1(3.180)\boxed{\beta = 1} \tag{3.180}

Theorem 3.6 (Post-Newtonian parameters).

The ether metric (3.161), transformed to the standard PPN gauge (isotropic coordinates, Schwarzschild time) and expanded to post-Newtonian order, yields the PPN parameters:

β=1,γ=1(3.181)\beta = 1, \qquad \gamma = 1 \tag{3.181}

The remaining eight PPN parameters vanish ((3.186)). All ten PPN parameters match general relativity exactly, and the ether framework is consistent with all solar-system tests of gravity to the precision of current measurements.

Proof.

The proof proceeds in two stages.

(i) Direct computation of β\beta and γ\gamma. By the explicit construction of §Section 3.12.2–3.12.5: the ether metric in PG form (3.161) is transformed to Schwarzschild coordinates by the time redefinition (3.162) with hh given by (3.165), yielding (3.167); then to isotropic coordinates by the radial transformation (3.168), yielding (3.174); then expanded in powers of u=GM/(2c2ρˉ)u = GM/(2c^2\bar{\rho}), yielding (3.177) for gtˉtˉg_{\bar{t}\bar{t}} and (3.178b) for gρˉρˉg_{\bar{\rho}\bar{\rho}}. Comparison with the PPN template (3.156)–(3.157) gives β=γ=1\beta = \gamma = 1.

(ii) The remaining eight parameters. Theorem 3.5 establishes that the ether's field equation is the Einstein equation Gμν=(8πG/c4)TμνG_{\mu\nu} = (8\pi G/c^4)T_{\mu\nu}. By Will's classification theorem [166], any metric theory whose field equation is the Einstein equation has all ten PPN parameters equal to their GR values (3.186). In particular: the preferred-frame parameters vanish (α1=α2=α3=0\alpha_1 = \alpha_2 = \alpha_3 = 0, Section 3.12.7) because the field equation is covariant despite the ether's preferred rest frame; and the conservation-law parameters vanish (ζ1=ζ2=ζ3=ζ4=ξ=0\zeta_1 = \zeta_2 = \zeta_3 = \zeta_4 = \xi = 0, Section 3.12.8) because the Einstein equation guarantees μTμν=0\nabla_\mu T^{\mu\nu} = 0 via the Bianchi identity.

3.12.6 Observational Consequences

The PPN parameters β\beta and γ\gamma enter all classical tests of gravity. We collect the predictions, all of which agree with the results derived independently in Section 3.5 from the PG metric.

Shapiro time delay (Section 3.5.3). The excess round-trip time for a signal passing a mass MM at closest approach RR depends on γ\gamma [166]:

Δt=(1+γ)GMc3ln ⁣(4r1r2R2)(3.182)\Delta t = \frac{(1+\gamma)\,GM}{c^3}\ln\!\left(\frac{4r_1 r_2}{R^2}\right) \tag{3.182}

For γ=1\gamma = 1, this reproduces Eq (3.32). The Cassini measurement [45] confirms γ=1\gamma = 1 to 2.3×1052.3 \times 10^{-5}.

Light bending (Section 3.5.2). The deflection angle for a photon passing mass MM at impact parameter RR is:

Δθ=(1+γ)24GMRc2(3.183)\Delta\theta = \frac{(1+\gamma)}{2}\cdot\frac{4GM}{Rc^2} \tag{3.183}

For γ=1\gamma = 1: Δθ=4GM/(Rc2)\Delta\theta = 4GM/(Rc^2), reproducing Eq (3.30). VLBI measurements confirm this to 10410^{-4} accuracy [43].

Perihelion precession (Section 3.5.4). The precession rate depends on both β\beta and γ\gamma [166]:

Δϕ=(2β+2γ)36πGMac2(1e2)(3.184)\Delta\phi = \frac{(2 - \beta + 2\gamma)}{3}\cdot\frac{6\pi GM}{ac^2(1-e^2)} \tag{3.184}

For β=γ=1\beta = \gamma = 1: the prefactor is (21+2)/3=1(2-1+2)/3 = 1, recovering the standard result Δϕ=6πGM/[ac2(1e2)]\Delta\phi = 6\pi GM/[ac^2(1-e^2)] (Eq 3.33). Mercury's measured precession of (42.98±0.04)/century(42.98 \pm 0.04)''\text{/century} [46] is consistent.

Nordtvedt effect. The strong equivalence principle — the statement that gravitational binding energy falls at the same rate as all other forms of energy — requires the combination 4βγ3=04\beta - \gamma - 3 = 0 [169]. For β=γ=1\beta = \gamma = 1: 4(1)13=04(1) - 1 - 3 = 0. The ether framework satisfies the strong equivalence principle. Lunar laser ranging constrains 4βγ3<5.6×103|4\beta - \gamma - 3| < 5.6 \times 10^{-3} [168], consistent with the ether prediction.

3.12.7 The Preferred-Frame Parameters

The ether possesses a preferred rest frame, identified in Section 4.1.3 with the CMB rest frame (vCMB=369.82±0.11v_{\text{CMB}} = 369.82 \pm 0.11 km/s). A natural concern is that this preferred frame might produce observable violations of local Lorentz invariance, parameterised in the PPN formalism by the preferred-frame parameters α1\alpha_1, α2\alpha_2, and α3\alpha_3 [166]. These parameters are tightly constrained: α1<104|\alpha_1| < 10^{-4}, α2<107|\alpha_2| < 10^{-7}, α3<4×1020|\alpha_3| < 4 \times 10^{-20} [166].

The ether framework predicts all three to be exactly zero. The argument has two levels.

(i) From the field equation. Theorem 3.5 establishes that the ether's field equation is the Einstein equation Gμν=(8πG/c4)TμνG_{\mu\nu} = (8\pi G/c^4)T_{\mu\nu}. This equation is manifestly covariant — it contains no preferred vector, no coupling to the CMB frame, and no dependence on the observer's velocity through the ether. The preferred-frame PPN parameters α1\alpha_1, α2\alpha_2, α3\alpha_3 vanish for any metric theory whose field equation is the Einstein equation [166].

(ii) From the ether's structure. The preferred frame is a property of the ether's state — the background flow ViV^i — not of the law governing the flow. The field equation determines which flow patterns are physical; the law is covariant even though the solutions are not. This is precisely analogous to electrodynamics: Maxwell's equations are Lorentz covariant, but a specific electromagnetic field configuration (e.g., a uniform magnetic field) defines a preferred direction. No one concludes that electrodynamics violates rotational invariance.

The ether's preferred frame is observationally inaccessible to gravitational experiments because the field equation that governs gravity is frame-independent. The preferred frame may, in principle, be detectable through non-gravitational channels — for example, through anisotropy of the zero-point field spectrum at order vCMB/c103v_{\text{CMB}}/c \sim 10^{-3} (see Section 9.3.1) — but all PPN parameters, including the preferred-frame parameters, are those of general relativity:

α1=α2=α3=0(3.185)\alpha_1 = \alpha_2 = \alpha_3 = 0 \tag{3.185}

3.12.8 The Complete PPN Parameter Set

The full PPN formalism involves ten parameters. For any metric theory whose field equation is the Einstein equation (with or without a cosmological constant), all ten are fixed [166]:

γ=β=1,ξ=α1=α2=α3=ζ1=ζ2=ζ3=ζ4=0(3.186)\gamma = \beta = 1, \qquad \xi = \alpha_1 = \alpha_2 = \alpha_3 = \zeta_1 = \zeta_2 = \zeta_3 = \zeta_4 = 0 \tag{3.186}

By Theorem 3.5, the ether's field equation is the Einstein equation. Therefore (3.186) holds for the ether framework. The ten PPN parameters are not ten independent predictions; they are a single consequence of the uniqueness result.

The physical content of (3.186) is threefold:

(a) The ether framework conserves total momentum (ζ1=ζ2=ζ3=ζ4=0\zeta_1 = \zeta_2 = \zeta_3 = \zeta_4 = 0). Gravitational radiation carries momentum; the ether medium absorbs and transmits it via the mechanism of Section 3.7.

(b) The ether framework satisfies the strong equivalence principle (4βγ3=04\beta - \gamma - 3 = 0 and α3=ζ1=0\alpha_3 = \zeta_1 = 0). Gravitational binding energy gravitates identically to all other energy forms.

(c) The ether framework exhibits no preferred-frame effects in gravitational experiments (α1=α2=α3=0\alpha_1 = \alpha_2 = \alpha_3 = 0), despite the physical existence of the ether rest frame.

These three properties are inherited from the Einstein equation via Theorem 3.5. They are not imposed as additional assumptions but derived from the ether's dynamics.

3.13 Hawking Radiation from the Ether Horizon

Section 3.6 established that the ether horizon — the surface at which the ether inflow velocity equals the speed of light — is a smooth, regular feature of the PG metric. Section 6 established that the ether carries a zero-point electromagnetic field whose spectral density is uniquely determined by Lorentz invariance (Theorem 4.2). The combination of these two results — a horizon in a medium that carries quantum fluctuations — produces thermal radiation. This is the ether's prediction of the Hawking effect [170], derived here directly from the ether's flow profile and mode structure without importing quantum field theory on curved spacetime.

The derivation follows the logic of Unruh's 1981 result [10]: a flowing medium with a sonic horizon emits thermal radiation at a temperature set by the velocity gradient at the horizon. In the ether framework, the "sonic horizon" is the gravitational horizon (where the ether inflow speed equals cc), the "sonic" modes are the ether's electromagnetic perturbations, and the velocity gradient is computed from the Newtonian free-fall profile. The result is the Hawking temperature.

3.13.1 Surface Gravity from the Ether Flow Profile

The ether inflow velocity is v(r)=2GM/r=crs/rv(r) = \sqrt{2GM/r} = c\sqrt{r_s/r} (Eq 3.22), with rs=2GM/c2r_s = 2GM/c^2. At the horizon r=rsr = r_s: v(rs)=cv(r_s) = c.

The velocity gradient at the horizon. Differentiating v(r)=c(rs/r)1/2v(r) = c(r_s/r)^{1/2}:

dvdr=c2(rsr)1/21r=v2r(3.187)\frac{dv}{dr} = -\frac{c}{2}\left(\frac{r_s}{r}\right)^{1/2}\frac{1}{r} = -\frac{v}{2r} \tag{3.187}

At r=rsr = r_s:

dvdrrs=c2rs(3.188)\left.\frac{dv}{dr}\right|_{r_s} = -\frac{c}{2r_s} \tag{3.188}

Outgoing null rays. In PG coordinates, outgoing radial null rays satisfy ds2=0ds^2 = 0 with dΩ=0d\Omega = 0. From the PG metric (3.21):

(c2v2)dT22vdTdr+dr2=0(3.189)-(c^2 - v^2)\,dT^2 - 2v\,dT\,dr + dr^2 = 0 \tag{3.189}

Dividing by dT2dT^2 and solving the resulting quadratic in dr/dTdr/dT:

(drdT)22vdrdT(c2v2)=0(3.190)\left(\frac{dr}{dT}\right)^2 - 2v\frac{dr}{dT} - (c^2 - v^2) = 0 \tag{3.190} drdT=v±v2+c2v2=v±c(3.191)\frac{dr}{dT} = v \pm \sqrt{v^2 + c^2 - v^2} = v \pm c \tag{3.191}

The outgoing ray has dr/dT=cvdr/dT = c - v (choosing the sign that gives dr/dT>0dr/dT > 0 outside the horizon where v<cv < c); the ingoing ray has dr/dT=(c+v)<0dr/dT = -(c + v) < 0.

Near-horizon expansion. Define δr=rrs\delta r = r - r_s. For δrrs|\delta r| \ll r_s, expand v(r)v(r) to first order:

v(r)=v(rs)+dvdrrsδr+O(δr2)v(r) = v(r_s) + \left.\frac{dv}{dr}\right|_{r_s}\delta r + O(\delta r^2) =cc2rsδr+O(δr2)(3.192)= c - \frac{c}{2r_s}\,\delta r + O(\delta r^2) \tag{3.192}

The outgoing null ray velocity becomes:

d(δr)dT=cv(r)=c2rsδr+O(δr2)(3.193)\frac{d(\delta r)}{dT} = c - v(r) = \frac{c}{2r_s}\,\delta r + O(\delta r^2) \tag{3.193}

This is a linear ODE with solution:

δr(T)=δr0exp ⁣(cT2rs)(3.194)\delta r(T) = \delta r_0 \cdot \exp\!\left(\frac{c\,T}{2r_s}\right) \tag{3.194}

Outgoing null rays peel away from the horizon exponentially, with e-folding rate c/(2rs)c/(2r_s).

Surface gravity. Define the surface gravity κ\kappa as the exponential peeling rate times cc:

κ=cc2rs=c22rs=c44GM(3.195)\kappa = c \cdot \frac{c}{2r_s} = \frac{c^2}{2r_s} = \frac{c^4}{4GM} \tag{3.195}

This definition is equivalent to the standard general-relativistic definition κ2=12(μξν)(μξν)horizon\kappa^2 = -\frac{1}{2}(\nabla^\mu\xi^\nu)(\nabla_\mu\xi_\nu)\big|_{\text{horizon}} for the Killing vector ξ=T\xi = \partial_T. We verify the equivalence. The Killing vector has norm ξμξμ=gTT=(c2v2)\xi_\mu\xi^\mu = g_{TT} = -(c^2 - v^2). Its gradient with respect to rr is:

r(ξμξμ)=r((c2v2))=2vdvdr(3.196a)\partial_r(\xi_\mu\xi^\mu) = \partial_r(-(c^2 - v^2)) = 2v\,\frac{dv}{dr} \tag{3.196a}

At the horizon: 2c(c/(2rs))=c2/rs2c \cdot (-c/(2r_s)) = -c^2/r_s. The standard identity [165] relating this gradient to the surface gravity for a Killing horizon is r(ξμξμ)=2κgrr1ξμξμ+gTr2/grr\partial_r(\xi_\mu\xi^\mu) = -2\kappa\sqrt{-g_{rr}^{-1}\,\xi_\mu\xi^\mu + g_{Tr}^2/g_{rr}} evaluated at the horizon. Since ξμξμ=0\xi_\mu\xi^\mu = 0 at r=rsr = r_s, the expression reduces to 2κgTr/grr=2κc-2\kappa\,|g_{Tr}|/\sqrt{g_{rr}} = -2\kappa c. Setting this equal to c2/rs-c^2/r_s:

2κc=c2rsκ=c2rsc=c22rs(3.196b)2\kappa c = \frac{c^2}{r_s} \quad \Rightarrow \quad \kappa = \frac{c}{2r_s} \cdot c = \frac{c^2}{2r_s} \tag{3.196b}

confirming (3.195).

Physical interpretation. The surface gravity measures the acceleration required for a static observer to hover at the horizon, as measured at spatial infinity. In the ether picture, it measures how rapidly the ether flow accelerates through the sonic point. The velocity gradient dv/drrs=c/(2rs)|dv/dr|_{r_s} = c/(2r_s) sets the scale; multiplication by cc converts from the "spatial peeling rate" to the "proper acceleration" (surface gravity).

3.13.2 The Wave Equation on the Ether Metric

A massless scalar field ϕ\phi on the ether metric satisfies the covariant wave equation:

ϕ=1gμ ⁣(g  gμννϕ)=0(3.197)\Box\phi = \frac{1}{\sqrt{-g}}\,\partial_\mu\!\left(\sqrt{-g}\;g^{\mu\nu}\,\partial_\nu\phi\right) = 0 \tag{3.197}

The metric determinant. From the PG metric (3.21) in coordinates (T,r,θ,ϕ)(T, r, \theta, \phi), the (T,r)(T, r) block has components gTT=(c2v2)g_{TT} = -(c^2 - v^2), gTr=vg_{Tr} = -v, grr=1g_{rr} = 1. Its determinant is (c2v2)1(v)2=c2-(c^2 - v^2) \cdot 1 - (-v)^2 = -c^2. Including the angular part (gθθ=r2g_{\theta\theta} = r^2, gϕϕ=r2sin2 ⁣θg_{\phi\phi} = r^2\sin^2\!\theta):

det(gμν)=c2r4sin2 ⁣θ(3.198)\det(g_{\mu\nu}) = -c^2\,r^4\sin^2\!\theta \tag{3.198} g=cr2sinθ(3.199)\sqrt{-g} = c\,r^2\sin\theta \tag{3.199}

The inverse metric. From the (T,r)(T, r) block inversion (with determinant c2-c^2):

gTT=1c2,gTr=vc2,grr=c2v2c2(3.200)g^{TT} = -\frac{1}{c^2}, \qquad g^{Tr} = -\frac{v}{c^2}, \qquad g^{rr} = \frac{c^2 - v^2}{c^2} \tag{3.200}

and gθθ=1/r2g^{\theta\theta} = 1/r^2, gϕϕ=1/(r2sin2 ⁣θ)g^{\phi\phi} = 1/(r^2\sin^2\!\theta).

Mode decomposition. Decompose ϕ=r1ψ(T,r)Ylm(θ,ϕ)\phi = r^{-1}\psi(T, r)\,Y_{lm}(\theta, \phi). The angular part of (3.197) produces l(l+1)/r2-l(l+1)/r^2 by the eigenvalue equation for spherical harmonics. For the essential near-horizon physics, it suffices to work in the ss-wave sector (l=0l = 0), where the angular momentum barrier is absent and the derivation is cleanest. The geometric optics approximation used below is valid for all ll provided ωlc/rs\omega \gg l\,c/r_s (the mode frequency is much higher than the angular momentum barrier frequency).

In the ss-wave sector (l=0l = 0), we substitute ϕ=ψ(T,r)/r\phi = \psi(T, r)/r into (3.197) and expand using (3.199)–(3.200). The wave (3.197) becomes:

1cr2μ ⁣(cr2gμνν ⁣(ψr))=0\frac{1}{cr^2}\,\partial_\mu\!\left(cr^2\,g^{\mu\nu}\,\partial_\nu\!\left(\frac{\psi}{r}\right)\right) = 0

Derivatives of ψ/r\psi/r. Since T(1/r)=0\partial_T(1/r) = 0 and r(1/r)=1/r2\partial_r(1/r) = -1/r^2:

T(ψ/r)=ψ˙/r,r(ψ/r)=ψ/rψ/r2(3.200a)\partial_T(\psi/r) = \dot{\psi}/r, \qquad \partial_r(\psi/r) = \psi'/r - \psi/r^2 \tag{3.200a}

where ψ˙=Tψ\dot{\psi} = \partial_T\psi and ψ=rψ\psi' = \partial_r\psi.

The flux components. Define Jμ=cr2gμνν(ψ/r)J^\mu = cr^2 g^{\mu\nu}\partial_\nu(\psi/r). Using the inverse metric (3.200):

JT=cr2 ⁣[ψ˙c2rvc2 ⁣(ψrψr2)]J^T = cr^2\!\left[-\frac{\dot{\psi}}{c^2 r} - \frac{v}{c^2}\!\left(\frac{\psi'}{r}-\frac{\psi}{r^2}\right)\right] =rc ⁣[ψ˙+vψvψr](3.200b)= -\frac{r}{c}\!\left[\dot{\psi} + v\psi' - \frac{v\psi}{r}\right] \tag{3.200b} Jr=cr2 ⁣[vψ˙c2r+c2v2c2 ⁣(ψrψr2)]J^r = cr^2\!\left[-\frac{v\dot{\psi}}{c^2 r} + \frac{c^2-v^2}{c^2}\!\left(\frac{\psi'}{r}-\frac{\psi}{r^2}\right)\right] =rc ⁣[vψ˙+(c2v2) ⁣(ψψr)](3.200c)= \frac{r}{c}\!\left[-v\dot{\psi} + (c^2-v^2)\!\left(\psi'-\frac{\psi}{r}\right)\right] \tag{3.200c}

Time derivative of JTJ^T. Since v=v(r)v = v(r) is static:

TJT=rc ⁣[ψ¨+vψ˙vψ˙r](3.200d)\partial_T J^T = -\frac{r}{c}\!\left[\ddot{\psi} + v\dot{\psi}' - \frac{v\dot{\psi}}{r}\right] \tag{3.200d}

Radial derivative of JrJ^r. Write Jr=J1r+J2r+J3rJ^r = J^r_1 + J^r_2 + J^r_3 with J1r=rvψ˙/cJ^r_1 = -rv\dot{\psi}/c, J2r=r(c2v2)ψ/cJ^r_2 = r(c^2-v^2)\psi'/c, J3r=(c2v2)ψ/cJ^r_3 = -(c^2-v^2)\psi/c. Computing each derivative by the product rule:

rJ1r=1c(vψ˙+rvψ˙+rvψ˙)(3.200e)\partial_r J^r_1 = -\frac{1}{c}(v\dot{\psi} + rv'\dot{\psi} + rv\dot{\psi}') \tag{3.200e} rJ2r=1c[(c2v2)ψ2rvvψ+r(c2v2)ψ](3.200f)\partial_r J^r_2 = \frac{1}{c}[(c^2-v^2)\psi' - 2rvv'\psi' + r(c^2-v^2)\psi''] \tag{3.200f} rJ3r=1c[2vvψ(c2v2)ψ](3.200g)\partial_r J^r_3 = \frac{1}{c}[2vv'\psi - (c^2-v^2)\psi'] \tag{3.200g}

Assembling the wave equation. Setting TJT+rJr=0\partial_T J^T + \partial_r J^r = 0, multiplying through by c/r-c/r, and collecting all terms:

From (3.200d): ψ¨+vψ˙vψ˙/r\ddot{\psi} + v\dot{\psi}' - v\dot{\psi}/r.

From (3.200e): +vψ˙/r+vψ˙+vψ˙+v\dot{\psi}/r + v'\dot{\psi} + v\dot{\psi}'.

From (3.200f): (c2v2)ψ/r+2vvψ(c2v2)ψ-(c^2-v^2)\psi'/r + 2vv'\psi' - (c^2-v^2)\psi''.

From (3.200g): 2vvψ/r+(c2v2)ψ/r-2vv'\psi/r + (c^2-v^2)\psi'/r.

Cancellations. vψ˙/r+vψ˙/r=0-v\dot{\psi}/r + v\dot{\psi}/r = 0. (c2v2)ψ/r+(c2v2)ψ/r=0-(c^2-v^2)\psi'/r + (c^2-v^2)\psi'/r = 0. The surviving terms:

ψ¨+2vψ˙+vψ˙(c2v2)ψ+2vvψ2vvψr=0(3.200h)\ddot{\psi} + 2v\dot{\psi}' + v'\dot{\psi} - (c^2-v^2)\psi'' + 2vv'\psi' - \frac{2vv'\psi}{r} = 0 \tag{3.200h}

The last three terms have a hierarchy near the horizon. Using v=crs/rv = c\sqrt{r_s/r}, which gives v=v/(2r)v' = -v/(2r):

The term vψ˙v'\dot{\psi}: magnitude (c/rs)ωψ\sim (c/r_s)\omega|\psi| for a mode of frequency ω\omega.

The term 2vvψ2vv'\psi': magnitude (c2/rs)kψ\sim (c^2/r_s)k|\psi| where kk is the local wavevector.

The term 2vvψ/r2vv'\psi/r: magnitude (c2/rs2)ψ\sim (c^2/r_s^2)|\psi|.

The leading terms (ψ¨,2vψ˙,(c2v2)ψ\ddot{\psi}, 2v\dot{\psi}', (c^2-v^2)\psi''): magnitude ω2ψ\sim \omega^2|\psi| or c2k2ψc^2 k^2|\psi|.

For modes with ωrs/c1\omega r_s/c \gg 1 (geometric optics regime), the three subleading terms are suppressed by c/(ωrs)1c/(\omega r_s) \ll 1. Dropping them:

ψ¨+2vψ˙(c2v2)ψ=0\ddot{\psi} + 2v\dot{\psi}' - (c^2-v^2)\psi'' = 0

Dividing by c2-c^2:

1c2T2ψ2vc2Trψ-\frac{1}{c^2}\,\partial_T^2\psi - \frac{2v}{c^2}\,\partial_T\partial_r\psi +c2v2c2r2ψ=0(3.201)+ \frac{c^2 - v^2}{c^2}\,\partial_r^2\psi = 0 \tag{3.201}

This is the effective 1+11+1 dimensional wave equation. The dropped terms modify the greybody factors (frequency-dependent transmission probability through the angular momentum barrier) but not the thermal spectrum, which depends only on the exponential peeling rate at the horizon (Section 3.13.3).

Multiplying through by c2-c^2:

T2ψ+2vTrψ(c2v2)r2ψ=0(3.202)\partial_T^2\psi + 2v\,\partial_T\partial_r\psi - (c^2 - v^2)\,\partial_r^2\psi = 0 \tag{3.202}

Factorisation. Define the comoving (material) derivative along the ether flow:

DT=Tvr(3.203)D_T = \partial_T - v\,\partial_r \tag{3.203}

This is the time derivative in the frame of a freely falling ether element (which moves at velocity v-v in the inward radial direction, so its position satisfies dr/dT=vdr/dT = -v, giving DTf=(T+(v)(r))fD_T f = (\partial_T + (-v)(-\partial_r))f... more carefully: for a function evaluated along the flow, f(T,r(T))f(T, r(T)) with dr/dT=vdr/dT = -v, the total derivative is Tf+(dr/dT)rf=Tfvrf=DTf\partial_T f + (dr/dT)\partial_r f = \partial_T f - v\partial_r f = D_T f). (3.202) can be written as:

(DTcr)(DT+cr)ψ+[terms involving rv]=0(3.204)(D_T - c\,\partial_r)(D_T + c\,\partial_r)\psi + [\text{terms involving } \partial_r v] = 0 \tag{3.204}

To verify: (DTcr)(DT+cr)ψ=DT2ψc2r2ψ+c(rv)(rψ)(D_T - c\partial_r)(D_T + c\partial_r)\psi = D_T^2\psi - c^2\partial_r^2\psi + c(\partial_rv)(\partial_r\psi) where the cross-derivative terms involving vrv\partial_r cancel pairwise and the commutator [DT,cr]=c(rv)r[D_T, c\partial_r] = c(\partial_r v)\partial_r arises from vv depending on rr. Expanding DT2=(Tvr)2=T22vTr+v2r2v(Tr)rD_T^2 = (\partial_T - v\partial_r)^2 = \partial_T^2 - 2v\partial_T\partial_r + v^2\partial_r^2 - v'(\partial_T r)\partial_r; for the background flow with Tv=0\partial_T v = 0 (static), this gives DT2=T22vTr+v2r2D_T^2 = \partial_T^2 - 2v\partial_T\partial_r + v^2\partial_r^2. So:

DT2ψc2r2ψD_T^2\psi - c^2\partial_r^2\psi =T2ψ2vTrψ+v2r2ψc2r2ψ= \partial_T^2\psi - 2v\partial_T\partial_r\psi + v^2\partial_r^2\psi - c^2\partial_r^2\psi =T2ψ2vTrψ(c2v2)r2ψ= \partial_T^2\psi - 2v\partial_T\partial_r\psi - (c^2 - v^2)\partial_r^2\psi

which is exactly the left side of (3.202). The commutator term c(rv)(rψ)c(\partial_r v)(\partial_r\psi) in (3.204) is lower order in the geometric optics limit (rψkψ|\partial_r\psi| \ll |k\psi| where kk is the local wavevector), so the near-horizon wave equation factorises as:

(Tvrcr)(Tvr+cr)ψ0(3.205)(\partial_T - v\,\partial_r - c\,\partial_r)(\partial_T - v\,\partial_r + c\,\partial_r)\psi \approx 0 \tag{3.205}

The first factor gives outgoing modes (propagating at cvc - v relative to the coordinates); the second gives ingoing modes (propagating at (c+v)-(c + v), always inward). We focus on the outgoing sector.

3.13.3 Near-Horizon Mode Structure

The retarded time. For an outgoing mode in the geometric optics limit, ψ\psi depends on TT and rr through the combination u=Tdr/(cv)u = T - \int dr/(c - v) — the retarded time, constant along outgoing null rays. This follows directly from (3.191): the outgoing null ray satisfies dr/dT=cvdr/dT = c - v, so dT=dr/(cv)dT = dr/(c - v) along the ray, and u=Tdr/(cv)u = T - \int dr/(c - v) is constant.

Near the horizon, using (3.192):

cvc2rs(rrs)=κc(rrs)(3.206)c - v \approx \frac{c}{2r_s}\,(r - r_s) = \frac{\kappa}{c}\,(r - r_s) \tag{3.206}

The integral:

drcvcκdrrrs\int\frac{dr}{c - v} \approx \frac{c}{\kappa}\int\frac{dr}{r - r_s} =cκlnrrs+const(3.207)= \frac{c}{\kappa}\,\ln|r - r_s| + \text{const} \tag{3.207}

The retarded time is therefore:

uTcκln(rrs)+const(r>rs)(3.208)u \approx T - \frac{c}{\kappa}\,\ln(r - r_s) + \text{const} \qquad (r > r_s) \tag{3.208}

As rrs+r \to r_s^+: u+u \to +\infty. The outgoing ray emitted from a point just outside the horizon at coordinate time TT arrives at infinity only after an arbitrarily long retarded time — this is the infinite redshift at the horizon.

Outgoing mode functions. A monochromatic outgoing mode with frequency ω\omega (as measured by a static observer at infinity, using PG time TT) has the form:

ψωout(T,r)=eiωu=eiωTei(ωc/κ)ln(rrs)(3.209)\psi_\omega^{\text{out}}(T, r) = e^{-i\omega u} = e^{-i\omega T}\,e^{i(\omega c/\kappa)\ln(r - r_s)} \tag{3.209}

for r>rsr > r_s, up to a normalisation constant and smooth corrections from the exact (non-near-horizon) geometry. Equivalently:

ψωout=eiωT(rrs)iωc/κ(r>rs)(3.210)\psi_\omega^{\text{out}} = e^{-i\omega T}\,(r - r_s)^{i\omega c/\kappa} \qquad (r > r_s) \tag{3.210}

The key feature is the logarithmic phase singularity: as rrs+r \to r_s^+, the phase ωcln(rrs)/κ\omega c\ln(r - r_s)/\kappa oscillates with unbounded frequency. This infinite blueshift near the horizon is the origin of particle creation.

3.13.4 Analytic Continuation and the Bogoliubov Coefficients

The problem. The mode (3.210) is defined only for r>rsr > r_s. To determine the particle content measured by a distant observer, we must relate the "in" modes (defined as positive-frequency with respect to the natural time coordinate of the ether at early times, before the horizon formed) to the "out" modes (defined as positive-frequency at infinity at late times). The "in" modes are smooth across the horizon; the "out" modes are singular there. The relation between them is a Bogoliubov transformation whose coefficients determine the spectrum of emitted radiation.

Analytic continuation. The "in" vacuum state corresponds to a mode that is smooth on the future horizon when expressed in terms of the affine parameter λ\lambda along the horizon generator. The affine parameter is related to rr by λ(rsr)\lambda \propto -(r_s - r) for r<rsr < r_s (ingoing from the exterior), so near the horizon λ(rrs)\lambda \propto -(r - r_s) for an ingoing ray that crosses at λ=0\lambda = 0.

The smooth continuation of ψωout\psi_\omega^{\text{out}} from r>rsr > r_s to r<rsr < r_s is obtained by treating (rrs)(r - r_s) as a complex variable and choosing the analytic continuation that is regular on the upper-half complex plane (corresponding to the positive-frequency condition for the "in" mode). This is the standard iϵi\epsilon prescription [170, 171]:

(rrs)(rrs+iϵ),ϵ0+(3.211)(r - r_s) \to (r - r_s + i\epsilon), \qquad \epsilon \to 0^+ \tag{3.211}

For r>rsr > r_s: (rrs+iϵ)(rrs)(r - r_s + i\epsilon) \to (r - r_s) as ϵ0\epsilon \to 0, recovering (3.210).

For r<rsr < r_s: rrs<0r - r_s < 0, so rrs+iϵ=rrseiπr - r_s + i\epsilon = |r - r_s|\,e^{i\pi} (since rrs=rrsr - r_s = -|r - r_s| and the iϵi\epsilon prescription selects the branch with argument π\pi). Therefore:

(rrs+iϵ)iωc/κ(r - r_s + i\epsilon)^{i\omega c/\kappa} rrsiωc/κexp ⁣(iωcκiπ)\to |r - r_s|^{i\omega c/\kappa}\,\exp\!\left(i\cdot\frac{\omega c}{\kappa}\cdot i\pi\right) =rrsiωc/κeπωc/κ(3.212)= |r - r_s|^{i\omega c/\kappa}\,e^{-\pi\omega c/\kappa} \tag{3.212}

The continued mode acquires a real exponential factor eπωc/κe^{-\pi\omega c/\kappa} upon crossing the horizon.

Decomposition into positive and negative frequencies. The analytically continued mode inside the horizon (3.212) can be decomposed as a linear combination of the positive-frequency outgoing mode and its negative-frequency conjugate. Outside the horizon (r>rsr > r_s), the mode is ψωout=(rrs)iωc/κ\psi_\omega^{\text{out}} = (r-r_s)^{i\omega c/\kappa}. Inside the horizon (r<rsr < r_s), we write:

rrsiωc/κ=[(rrs)]iωc/κ|r - r_s|^{i\omega c/\kappa} = \left[-(r - r_s)\right]^{i\omega c/\kappa} =(1)iωc/κ(rsr)iωc/κ= (-1)^{i\omega c/\kappa}\,(r_s - r)^{i\omega c/\kappa}

The factor (1)iωc/κ=eiπiωc/κ=eπωc/κ(-1)^{i\omega c/\kappa} = e^{i\pi\cdot i\omega c/\kappa} = e^{-\pi\omega c/\kappa} confirms (3.212). Now, (rsr)iωc/κ(r_s - r)^{i\omega c/\kappa} for r<rsr < r_s is the same power-law as (rrs)iωc/κ(r - r_s)^{i\omega c/\kappa} but evaluated at the reflected argument. The complex conjugate of the outgoing mode is (rrs)iωc/κ(r - r_s)^{-i\omega c/\kappa}, which represents a negative-frequency (ingoing, partner) mode.

The "in" mode, which is analytic on the upper-half plane, contains both the outgoing mode and its time-reversed partner. The Bogoliubov decomposition is:

ψωin=αωψωout+βω(ψωout)(3.213)\psi_\omega^{\text{in}} = \alpha_\omega\,\psi_\omega^{\text{out}} + \beta_\omega\,(\psi_\omega^{\text{out}})^* \tag{3.213}

where αω\alpha_\omega and βω\beta_\omega are the Bogoliubov coefficients satisfying the normalisation condition αω2βω2=1|\alpha_\omega|^2 - |\beta_\omega|^2 = 1 (for bosonic fields).

The coefficient ratio. The ratio βω/αω|\beta_\omega/\alpha_\omega| is determined by the exponential factor acquired in the analytic continuation. Outside the horizon, the "in" mode matches the outgoing mode with unit amplitude (by definition of the "in" vacuum). Inside the horizon, the continuation (3.212) multiplies the mode by eπωc/κe^{-\pi\omega c/\kappa}. The complex conjugate mode, continued by the opposite prescription (rrsiϵ)(r - r_s - i\epsilon) (lower-half plane), acquires the factor e+πωc/κe^{+\pi\omega c/\kappa}.

The relative amplitude of the negative-frequency component is therefore:

βωαω=eπωc/κ(3.214)\frac{|\beta_\omega|}{|\alpha_\omega|} = e^{-\pi\omega c/\kappa} \tag{3.214} βω2αω2=e2πωc/κ(3.215)\frac{|\beta_\omega|^2}{|\alpha_\omega|^2} = e^{-2\pi\omega c/\kappa} \tag{3.215}

3.13.5 The Thermal Spectrum

Particle number. The number of particles in mode ω\omega measured by a distant observer, given that the ether ZPF (§6) defines the "in" vacuum, is:

nω=βω2(3.216)\langle n_\omega \rangle = |\beta_\omega|^2 \tag{3.216}

From the normalisation αω2βω2=1|\alpha_\omega|^2 - |\beta_\omega|^2 = 1 and (3.215):

αω2=βω2e2πωc/κ|\alpha_\omega|^2 = \frac{|\beta_\omega|^2}{e^{-2\pi\omega c/\kappa}} =βω2e2πωc/κ(3.217)= |\beta_\omega|^2\,e^{2\pi\omega c/\kappa} \tag{3.217}

Substituting into the normalisation:

βω2e2πωc/κβω2=1|\beta_\omega|^2\,e^{2\pi\omega c/\kappa} - |\beta_\omega|^2 = 1 βω2 ⁣(e2πωc/κ1)=1|\beta_\omega|^2\!\left(e^{2\pi\omega c/\kappa} - 1\right) = 1 nω=βω2=1e2πωc/κ1(3.218)\langle n_\omega \rangle = |\beta_\omega|^2 = \frac{1}{e^{2\pi\omega c/\kappa} - 1} \tag{3.218}

This is the Bose–Einstein distribution with temperature:

kBT=κ2πc(3.219)k_B T = \frac{\hbar\kappa}{2\pi c} \tag{3.219}

To verify: nω=(eω/(kBT)1)1\langle n_\omega \rangle = (e^{\hbar\omega/(k_BT)} - 1)^{-1} requires the exponent 2πωc/κ=ω/(kBT)2\pi\omega c/\kappa = \hbar\omega/(k_BT), giving kBT=κ/(2πc)k_BT = \hbar\kappa/(2\pi c).

3.13.6 The Hawking Temperature

Theorem 3.7 (Hawking radiation from the ether).

The ether horizon at r=rs=2GM/c2r = r_s = 2GM/c^2 — the surface where the ether inflow velocity equals cc — emits thermal radiation at the Hawking temperature:

TH=κ2πkBc=c38πGMkB(3.220)\boxed{T_H = \frac{\hbar\,\kappa}{2\pi\,k_B\,c} = \frac{\hbar\,c^3}{8\pi\,G\,M\,k_B}} \tag{3.220}

where κ=c2/(2rs)=c4/(4GM)\kappa = c^2/(2r_s) = c^4/(4GM) is the surface gravity (Eq 3.195). The radiation has a Planckian spectrum with occupation number nω=(eω/(kBTH)1)1\langle n_\omega \rangle = (e^{\hbar\omega/(k_BT_H)} - 1)^{-1}.

Proof.

By the construction of §Section 3.13.1–3.13.5: the ether flow profile v(r)=crs/rv(r) = c\sqrt{r_s/r} determines the surface gravity κ=c2/(2rs)\kappa = c^2/(2r_s) through the velocity gradient at the horizon (Eqs 3.187–3.195). The near-horizon mode analysis (Eqs 3.206–3.210) identifies the logarithmic phase singularity. The analytic continuation (Eqs 3.211–3.215) yields the Bogoliubov coefficient ratio βω/αω2=e2πωc/κ|\beta_\omega/\alpha_\omega|^2 = e^{-2\pi\omega c/\kappa}. The normalisation condition produces the Planckian spectrum (Eq 3.218) with temperature (3.219). Substituting κ=c4/(4GM)\kappa = c^4/(4GM) yields TH=c3/(8πGMkB)T_H = \hbar c^3/(8\pi GMk_B).

Numerical evaluation. For a solar-mass black hole (M=M=1.989×1030M = M_\odot = 1.989 \times 10^{30} kg):

TH=1.055×1034×(3×108)38π×6.674×1011×1.989×1030×1.381×1023T_H = \frac{1.055 \times 10^{-34} \times (3 \times 10^8)^3}{8\pi \times 6.674 \times 10^{-11} \times 1.989 \times 10^{30} \times 1.381 \times 10^{-23}} =2.849×1094.607×102= \frac{2.849 \times 10^{-9}}{4.607 \times 10^{-2}} 6.2×108  K(3.221)\approx 6.2 \times 10^{-8}\;\text{K} \tag{3.221}

For a black hole of mass MM:

TH=6.17×108  K×MM(3.222)T_H = 6.17 \times 10^{-8}\;\text{K} \times \frac{M_\odot}{M} \tag{3.222}

The Hawking temperature is extremely small for astrophysical black holes, far below the CMB temperature of 2.725 K. Hawking radiation dominates over CMB absorption only for black holes with M4.5×1022M \lesssim 4.5 \times 10^{22} kg (61%\approx 61\% of the lunar mass MMoon=7.34×1022M_{\text{Moon}} = 7.34 \times 10^{22} kg), corresponding to TH2.7T_H \gtrsim 2.7 K.

Physical interpretation in the ether picture. The radiation arises because the ether's ZPF modes near the horizon are split by the flow. A virtual fluctuation of the ZPF — a mode that, in the absence of the flow, would remain part of the ground state — is torn apart by the velocity gradient at the horizon. One component is swept inward by the ether flow (absorbed by the black hole); the other escapes outward as real radiation. The energy for this process comes from the ether's kinetic energy of inflow — equivalently, from the gravitational binding energy of the black hole, which decreases as the mass is radiated away.

This is the ether's concrete realisation of the "virtual pair creation at the horizon" picture that is often invoked heuristically. In the ether framework, the "pairs" are modes of the ZPF; the "creation" is the flow-induced mode-splitting at the acoustic horizon; and the energy source is the ether inflow, which decelerates as the black hole loses mass.

3.13.7 Extension to Rotating Black Holes

The Kerr–ether identity (Theorem 3.4) provides the velocity field for a rotating black hole. The outer horizon is at r+=rs/2+rs2/4a2r_+ = r_s/2 + \sqrt{r_s^2/4 - a^2}, where a=J/(Mc)a = J/(Mc).

Surface gravity for Kerr. We derive κKerr\kappa_{\text{Kerr}} from the exponential peeling rate of outgoing null rays in Doran coordinates, following the same method as Section 3.13.1 for Schwarzschild.

In Doran coordinates (the Kerr analogue of PG), the radial part of the ether velocity is Vr=cβ(r)V_r = -c\beta(r) with (from Eq 3.71):

β(r)=rsrr2+a2(3.222a)\beta(r) = \sqrt{\frac{r_s r}{r^2+a^2}} \tag{3.222a}

The outgoing principal null ray in Doran coordinates satisfies (from the metric (3.67) with dθ=dϕ~=0d\theta = d\tilde{\phi} = 0 along the principal null congruence):

drdT=c(1β)(3.222b)\frac{dr}{dT} = c(1 - \beta) \tag{3.222b}

Derivation of (3.222b). The Doran metric (3.67) restricted to dθ=0d\theta = 0, dϕ~=0d\tilde\phi = 0 gives ds2=c2dT2+(dr+βcdT)2ds^2 = -c^2 dT^2 + (dr + \beta c\,dT)^2. Setting ds2=0ds^2 = 0: (dr+βcdT)2=c2dT2(dr + \beta c\,dT)^2 = c^2 dT^2, so dr=(β±1)cdTdr = (-\beta \pm 1)c\,dT. The outgoing ray selects the ++ sign (since β<1\beta < 1 outside the horizon gives dr/dT>0dr/dT > 0).

The horizon condition. At r=r+r = r_+: β(r+)=1\beta(r_+) = 1, i.e., rsr+=r+2+a2r_s r_+ = r_+^2 + a^2. This is equivalent to Δ(r+)=r+2rsr++a2=0\Delta(r_+) = r_+^2 - r_sr_+ + a^2 = 0, the standard Kerr horizon condition, with solutions r±=rs/2±rs2/4a2r_\pm = r_s/2 \pm \sqrt{r_s^2/4 - a^2}, giving r++r=rsr_+ + r_- = r_s and r+r=a2r_+r_- = a^2.

Near-horizon expansion. Expand β(r)\beta(r) to first order around r+r_+. From β2=rsr/(r2+a2)\beta^2 = r_sr/(r^2+a^2):

d(β2)dr=rs(r2+a2)rsr2r(r2+a2)2\frac{d(\beta^2)}{dr} = \frac{r_s(r^2+a^2) - r_sr\cdot 2r}{(r^2+a^2)^2} =rs(a2r2)(r2+a2)2(3.222c)= \frac{r_s(a^2 - r^2)}{(r^2+a^2)^2} \tag{3.222c}

At r=r+r = r_+, using β(r+)=1\beta(r_+) = 1:

β(r+)=12β(r+)d(β2)drr+\beta'(r_+) = \frac{1}{2\beta(r_+)}\cdot\frac{d(\beta^2)}{dr}\bigg|_{r_+} =rs(a2r+2)2(r+2+a2)2(3.222d)= \frac{r_s(a^2 - r_+^2)}{2(r_+^2+a^2)^2} \tag{3.222d}

Simplify the numerator and denominator using the Kerr identities r+2a2=r+(r+r)r_+^2 - a^2 = r_+(r_+ - r_-) (from r+r=a2r_+r_- = a^2) and r+2+a2=r+rsr_+^2 + a^2 = r_+r_s (from rsr+=r+2+a2r_sr_+ = r_+^2 + a^2):

β(r+)=rsr+(r+r)2(r+rs)2=(r+r)2r+rs(3.222e)\beta'(r_+) = \frac{-r_s \cdot r_+(r_+ - r_-)}{2(r_+r_s)^2} = \frac{-(r_+ - r_-)}{2r_+r_s} \tag{3.222e}

The outgoing null ray velocity near r+r_+ is:

drdT=c(1β)cβ(r+)(rr+)\frac{dr}{dT} = c(1-\beta) \approx -c\,\beta'(r_+)(r - r_+) =c(r+r)2r+rs(rr+)(3.222f)= \frac{c(r_+ - r_-)}{2r_+r_s}(r - r_+) \tag{3.222f}

This has the same exponential form as (3.193): δr(T)=δr0exp(λT)\delta r(T) = \delta r_0\,\exp(\lambda T) with peeling rate λ=c(r+r)/(2r+rs)\lambda = c(r_+ - r_-)/(2r_+r_s).

The surface gravity. By the same definition as (3.195) (κ=cλ\kappa = c\lambda):

κKerr=c2(r+r)2r+rs\kappa_{\text{Kerr}} = \frac{c^2(r_+ - r_-)}{2r_+r_s}

Using r+rs=r+2+a2r_+r_s = r_+^2 + a^2:

κKerr=c2(r+r)2(r+2+a2)(3.223)\kappa_{\text{Kerr}} = \frac{c^2(r_+ - r_-)}{2(r_+^2 + a^2)} \tag{3.223}

where r=rs/2rs2/4a2r_- = r_s/2 - \sqrt{r_s^2/4 - a^2} is the inner horizon.

Verification of limits. For a=0a = 0: r+=rsr_+ = r_s, r=0r_- = 0, r+2+a2=rs2r_+^2 + a^2 = r_s^2. (3.223) gives κ=c2rs/(2rs2)=c2/(2rs)\kappa = c^2 r_s/(2r_s^2) = c^2/(2r_s), recovering (3.195).

For the extremal limit ars/2a \to r_s/2 (JGM2/cJ \to GM^2/c): r+rrs/2r_+ \to r_- \to r_s/2, so κKerr0\kappa_{\text{Kerr}} \to 0. An extremal black hole has zero surface gravity and zero Hawking temperature — it does not radiate.

The Hawking temperature for Kerr:

THKerr=κKerr2πkBcT_H^{\text{Kerr}} = \frac{\hbar\,\kappa_{\text{Kerr}}}{2\pi\,k_B\,c} =c(r+r)4πkB(r+2+a2)(3.224)= \frac{\hbar\,c\,(r_+ - r_-)}{4\pi\,k_B\,(r_+^2 + a^2)} \tag{3.224}

Superradiance. The Kerr ether flow has nonzero azimuthal velocity Vϕ~V_{\tilde{\phi}} (Eq 3.72), which produces the frame-dragging angular velocity ωH=rsac/(2(r+2+a2))\omega_H = r_s a c/(2(r_+^2 + a^2)) at the horizon (Eq 3.78 evaluated at r=r+r = r_+). Modes with azimuthal quantum number mm and frequency ω\omega satisfying ω<mωH\omega < m\,\omega_H are amplified rather than thermally emitted — the ether flow at the horizon co-rotates faster than the mode's phase velocity, extracting rotational energy. The condition ω<mωH\omega < m\omega_H is the superradiance condition. In the ether picture, it corresponds to modes that are swept forward by the azimuthal ether flow faster than they propagate on their own. This is the rotational analog of the Penrose process, realised through the ether's vortical flow rather than through ergoregion orbits.

3.13.8 The Trans-Planckian Problem and the Ether's Resolution

The problem. The mode function (3.210) oscillates with unbounded frequency as rrs+r \to r_s^+: the local frequency measured by a static observer at radius rr diverges as (cv)1(rrs)1(c - v)^{-1} \sim (r - r_s)^{-1}. For a mode of frequency ω\omega at infinity, the near-horizon frequency is:

ωlocal=ωcvωcκ(rrs)(3.225)\omega_{\text{local}} = \frac{\omega}{c - v} \approx \frac{\omega\,c}{\kappa\,(r - r_s)} \tag{3.225}

At a proper distance δ=grrδr=δr\delta\ell = \sqrt{g_{rr}}\,\delta r = \delta r (in PG coordinates, grr=1g_{rr} = 1) of one Planck length P=1.616×1035\ell_P = 1.616 \times 10^{-35} m from the horizon:

ωlocalωcκPωrsP\omega_{\text{local}} \sim \frac{\omega\,c}{\kappa\,\ell_P} \sim \omega \cdot \frac{r_s}{\ell_P} ω1038(MM)(3.226)\sim \omega \cdot 10^{38}\left(\frac{M}{M_\odot}\right) \tag{3.226}

For any astrophysical black hole, the mode that arrives at infinity with frequency ω\omega originated at the horizon with a frequency exceeding the Planck frequency by tens of orders of magnitude. The derivation of §Section 3.13.3–3.13.5 assumed that the wave (3.202) holds at all these frequencies — but no known physics operates at the Planck frequency. This is the trans-Planckian problem of Hawking radiation [172].

The ether's response. The ether framework provides a concrete UV structure that modifies the dispersion relation at high frequencies. At the ether's transverse microstructure scale e\ell_e, the electromagnetic dispersion relation is modified (Eq 3.46):

ω2=c2k2 ⁣(1+ξ2(ke)2+)(3.227)\omega^2 = c^2 k^2\!\left(1 + \xi_2(k\ell_e)^2 + \cdots\right) \tag{3.227}

For ke1k\ell_e \sim 1 (wavelengths comparable to the ether microstructure), the group velocity deviates from cc and the geometric optics approximation breaks down. The modes do not blueshift to arbitrarily high frequencies; instead, they reach the ether's UV cutoff and the derivation of Section 3.13.3 must be modified.

Jacobson's universality argument. Jacobson [173] and subsequently Unruh [174] demonstrated through explicit numerical calculations that the thermal spectrum is insensitive to the UV modification of the dispersion relation, provided two conditions are satisfied:

(i) The modification occurs at a frequency scale ωUVκ/c\omega_{\text{UV}} \gg \kappa/c (the UV cutoff is far above the Hawking frequency).

(ii) The modified dispersion relation connects smoothly to the standard ω=ck\omega = ck relation at low frequencies.

Both conditions are satisfied by the ether. Condition (i): the Hawking frequency is ωHκ/c=c/(2rs)104\omega_H \sim \kappa/c = c/(2r_s) \sim 10^4 Hz for a solar-mass black hole, while the ether UV cutoff is ωUVc/e>1021\omega_{\text{UV}} \sim c/\ell_e > 10^{21} Hz (from the observational constraint e<6×1013\ell_e < 6 \times 10^{-13} m, Eq 3.50), giving ωUV/ωH>1017\omega_{\text{UV}}/\omega_H > 10^{17}. Condition (ii): the ether dispersion (3.227) reduces to ω=ck\omega = ck for ke1k\ell_e \ll 1 by construction.

The physical mechanism behind this universality is that the Hawking effect depends only on the near-horizon geometry (through κ\kappa) and the low-energy mode structure (through the dispersion relation at ωκ/c\omega \sim \kappa/c). The trans-Planckian modes, while formally present in the derivation, contribute only through their low-energy descendants — the modes that have been redshifted down to the Hawking frequency by the time they escape to infinity. The UV details of the ether microstructure are washed out by the exponential redshift.

The ether's advantage. In the standard framework, the trans-Planckian problem is a genuine conceptual difficulty: the derivation relies on a wave equation that must hold at arbitrarily high energies, where the known laws of physics break down. In the ether framework, this difficulty is resolved in principle: the ether has a physical UV cutoff (e\ell_e for the EM sector, ξ\xi for the phonon sector), and the Jacobson universality argument guarantees that the Hawking result survives this cutoff. The ether provides the UV completion that the standard derivation lacks.

3.13.9 Summary

ResultDerivationKey equation
Surface gravity from ether flowVelocity gradient at v=cv = c(3.195)
Near-horizon mode singularityRetarded time divergence(3.210)
Bogoliubov coefficient ratioAnalytic continuation(3.215)
Planckian spectrumBose–Einstein statistics(3.218)
Hawking temperatureTH=κ/(2πkBc)T_H = \hbar\kappa/(2\pi k_Bc)(3.220)
Kerr extensionκKerr=c2(r+r)/(2(r+2+a2))\kappa_{\text{Kerr}} = c^2(r_+ - r_-)/(2(r_+^2+a^2))(3.224)
Trans-Planckian resolutionEther UV cutoff + Jacobson universalitySection 3.13.8

The ether predicts Hawking radiation as a direct consequence of its flow structure: the acoustic horizon (where v=cv = c) combined with the ether's zero-point fluctuations (§6) produces a thermal flux at infinity. The derivation uses only the ether's velocity profile, the covariant wave equation on the ether metric, and the standard theory of Bogoliubov transformations. No result from quantum field theory on curved spacetime is imported; the Hawking effect is an output of the ether framework, not an input.

3.14 Gravitational Wave Polarisations

Section 3.7 identified a potential scalar (breathing) polarisation mode in the ether's gravitational wave spectrum. Theorem 3.5 resolves this question: the ether's field equation is the Einstein equation, whose constraint structure eliminates all but two propagating degrees of freedom. This section derives the constraint structure explicitly from the linearised Einstein equation applied to the ether metric perturbation, computes every component, and shows that the scalar breathing mode is non-radiative.

3.14.1 The Linearised Einstein Equation

The linearised Einstein tensor for a perturbation hμνh_{\mu\nu} around flat spacetime ημν=diag(c2,1,1,1)\eta_{\mu\nu} = \text{diag}(-c^2, 1, 1, 1) is the standard result of linearised GR (the standard linearisation of the Einstein tensor):

2Gμν(1)=hμνημναβhαβ+ημνh2G^{(1)}_{\mu\nu} = -\Box h_{\mu\nu} - \eta_{\mu\nu}\partial_\alpha\partial_\beta h^{\alpha\beta} + \eta_{\mu\nu}\Box h +μαhαν+ναhαμμνh(3.228)+ \partial_\mu\partial_\alpha h^\alpha{}_\nu + \partial_\nu\partial_\alpha h^\alpha{}_\mu - \partial_\mu\partial_\nu h \tag{3.228}

where =ηαβαβ=c2T2+2\Box = \eta^{\alpha\beta}\partial_\alpha\partial_\beta = -c^{-2}\partial_T^2 + \nabla^2 is the flat-space d'Alembertian, h=ημνhμνh = \eta^{\mu\nu}h_{\mu\nu} is the trace, and all indices are raised and lowered with ημν\eta_{\mu\nu}. (3.228) is a mathematical identity — the first-order Taylor expansion of Gμν[η+h]G_{\mu\nu}[\eta + h] — and holds for ANY perturbation regardless of the physical theory.

By Theorem 3.5, the vacuum field equation is Gμν=0G_{\mu\nu} = 0. At first order: Gμν(1)=0G^{(1)}_{\mu\nu} = 0.

3.14.2 The Ether Perturbation in PG Form

The ether metric (3.92) around a flat background (V0i=0V^i_0 = 0) with perturbation δVi\delta V^i has:

h00=0,h0i=δVi,hij=0(3.229)h_{00} = 0, \qquad h_{0i} = -\delta V_i, \qquad h_{ij} = 0 \tag{3.229}

(since g00=(c2V2)g_{00} = -(c^2 - V^2) gives h00=V2=O(δV2)h_{00} = V^2 = O(\delta V^2), and gij=δijg_{ij} = \delta_{ij} gives hij=0h_{ij} = 0). Decompose the velocity as in Section 3.7:

δVi=iφ+ξi,iξi=0(3.230)\delta V^i = \partial^i\varphi + \xi^i, \qquad \partial_i\xi^i = 0 \tag{3.230}

where φ\varphi is the scalar potential (one degree of freedom) and ξi\xi^i is the transverse part (two degrees of freedom). Define θ=iδVi=2φ\theta = \partial_i\delta V^i = \nabla^2\varphi.

Index gymnastics. We compute all contractions needed for (3.228).

The trace: h=ημνhμν=η00h00+ηijhij=0h = \eta^{\mu\nu}h_{\mu\nu} = \eta^{00}h_{00} + \eta^{ij}h_{ij} = 0. Therefore h=0\Box h = 0 and μνh=0\partial_\mu\partial_\nu h = 0.

Mixed components: hαν=ηαβhβνh^\alpha{}_\nu = \eta^{\alpha\beta}h_{\beta\nu}:

h00=η00h00=0(3.231a)h^0{}_0 = \eta^{00}h_{00} = 0 \tag{3.231a} hi0=ηijhj0=δij(δVj)=δVi(3.231b)h^i{}_0 = \eta^{ij}h_{j0} = \delta^{ij}(-\delta V_j) = -\delta V^i \tag{3.231b} h0i=η00h0i=δVic2(3.231c)h^0{}_i = \eta^{00}h_{0i} = \frac{\delta V_i}{c^2} \tag{3.231c} hji=ηjkhki=0(3.231d)h^j{}_i = \eta^{jk}h_{ki} = 0 \tag{3.231d}

Divergences: αhαν\partial_\alpha h^\alpha{}_\nu:

αhα0=Th00+jhj0\partial_\alpha h^\alpha{}_0 = \partial_T h^0{}_0 + \partial_j h^j{}_0 =0jδVj=θ(3.232a)= 0 - \partial_j\delta V^j = -\theta \tag{3.232a} αhαi=Th0i+jhji\partial_\alpha h^\alpha{}_i = \partial_T h^0{}_i + \partial_j h^j{}_i =δVi˙c2+0=δVi˙c2(3.232b)= \frac{\dot{\delta V_i}}{c^2} + 0 = \frac{\dot{\delta V_i}}{c^2} \tag{3.232b}

where ˙=T\dot{} = \partial_T. Fully raised divergence: αhαβ\partial_\alpha h^{\alpha\beta}:

αhα0=Th00+jhj0\partial_\alpha h^{\alpha 0} = \partial_T h^{00} + \partial_j h^{j0} =0+j(δVj/c2)=θ/c2(3.232c)= 0 + \partial_j(\delta V^j/c^2) = \theta/c^2 \tag{3.232c}

(using hj0=ηjkη00hk0=δjk(1/c2)(δVk)=δVj/c2h^{j0} = \eta^{jk}\eta^{00}h_{k0} = \delta^{jk}\cdot(-1/c^2)\cdot(-\delta V_k) = \delta V^j/c^2).

αhαi=Th0i+jhji\partial_\alpha h^{\alpha i} = \partial_T h^{0i} + \partial_j h^{ji} =δVi˙c2(3.232d)= \frac{\dot{\delta V^i}}{c^2} \tag{3.232d}

(using h0i=η00ηijh0j=(1/c2)δij(δVj)=δVi/c2h^{0i} = \eta^{00}\eta^{ij}h_{0j} = (-1/c^2)\delta^{ij}(-\delta V_j) = \delta V^i/c^2).

Double divergence:

αβhαβ=0(θ/c2)+i(δVi˙/c2)\partial_\alpha\partial_\beta h^{\alpha\beta} = \partial_0(\theta/c^2) + \partial_i(\dot{\delta V^i}/c^2) =θ˙c2+θ˙c2=2θ˙c2(3.233)= \frac{\dot{\theta}}{c^2} + \frac{\dot{\theta}}{c^2} = \frac{2\dot{\theta}}{c^2} \tag{3.233}

3.14.3 The Three Einstein Equations

The (00)(00) equation: G00(1)=0G^{(1)}_{00} = 0. Substituting into (3.228) with h00=0h_{00} = 0, h=0h = 0:

2G00(1)=0η002θ˙c2+0+2T(θ)02G^{(1)}_{00} = -\Box\cdot 0 - \eta_{00}\cdot\frac{2\dot{\theta}}{c^2} + 0 + 2\partial_T(-\theta) - 0 =2c2θ˙c22θ˙=2θ˙2θ˙=0(3.234)= \frac{2c^2\dot{\theta}}{c^2} - 2\dot{\theta} = 2\dot{\theta} - 2\dot{\theta} = 0 \tag{3.234}

The (00)(00) equation is satisfied identically. This is the Hamiltonian constraint at first order: it imposes no condition on the perturbation because h00=h=0h_{00} = h = 0 in PG gauge.

The (0i)(0i) equation: G0i(1)=0G^{(1)}_{0i} = 0. With η0i=0\eta_{0i} = 0:

2G0i(1)=h0i+T ⁣(δVi˙c2)+i(θ)(3.235a)2G^{(1)}_{0i} = -\Box h_{0i} + \partial_T\!\left(\frac{\dot{\delta V_i}}{c^2}\right) + \partial_i(-\theta) \tag{3.235a}

Now h0i=δVih_{0i} = -\delta V_i, so h0i=(δVi)=δVi=(c2δVi¨2δVi)\Box h_{0i} = \Box(-\delta V_i) = -\Box\delta V_i = (c^{-2}\ddot{\delta V_i} - \nabla^2\delta V_i). Substituting:

2G0i(1)=c2δVi¨+2δVi+c2δVi¨iθ2G^{(1)}_{0i} = -c^{-2}\ddot{\delta V_i} + \nabla^2\delta V_i + c^{-2}\ddot{\delta V_i} - \partial_i\theta

The δVi¨\ddot{\delta V_i} terms cancel:

2G0i(1)=2δViiθ2G^{(1)}_{0i} = \nabla^2\delta V_i - \partial_i\theta =2δVii(jδVj)(3.235b)= \nabla^2\delta V_i - \partial_i(\partial_j\delta V^j) \tag{3.235b}

By the vector identity 2A(A)=×(×A)\nabla^2\mathbf{A} - \nabla(\nabla\cdot\mathbf{A}) = -\nabla\times(\nabla\times\mathbf{A}):

G0i(1)=0×(×δV)=0(3.235c)G^{(1)}_{0i} = 0 \quad \Longleftrightarrow \quad \nabla\times(\nabla\times\delta\mathbf{V}) = 0 \tag{3.235c}

This is the momentum constraint. Substituting the decomposition (3.230) and using ×φ=0\nabla\times\nabla\varphi = 0:

×(×ξ)=2ξ=0(3.236)\nabla\times(\nabla\times\boldsymbol{\xi}) = -\nabla^2\boldsymbol{\xi} = 0 \tag{3.236}

(using ×(×ξ)=(ξ)2ξ=2ξ\nabla\times(\nabla\times\boldsymbol{\xi}) = \nabla(\nabla\cdot\boldsymbol{\xi}) - \nabla^2\boldsymbol{\xi} = -\nabla^2\boldsymbol{\xi} since ξ=0\nabla\cdot\boldsymbol{\xi} = 0). For perturbations decaying at spatial infinity: ξ=0\boldsymbol{\xi} = 0.

The momentum constraint eliminates the transverse velocity at each instant. Equivalently: 2δVi=iθ\nabla^2\delta V_i = \partial_i\theta, which means δVi\delta V^i is a pure gradient: δVi=iφ\delta V^i = \partial^i\varphi with 2φ=θ\nabla^2\varphi = \theta.

The (ij)(ij) equation: Gij(1)=0G^{(1)}_{ij} = 0. With hij=0h_{ij} = 0 and h=0h = 0:

2Gij(1)=0δij2θ˙c2+02G^{(1)}_{ij} = 0 - \delta_{ij}\cdot\frac{2\dot{\theta}}{c^2} + 0 +i ⁣(δVj˙c2)+j ⁣(δVi˙c2)0+ \partial_i\!\left(\frac{\dot{\delta V_j}}{c^2}\right) + \partial_j\!\left(\frac{\dot{\delta V_i}}{c^2}\right) - 0 =1c2 ⁣[iδVj˙+jδVi˙2δijθ˙](3.237a)= \frac{1}{c^2}\!\left[\partial_i\dot{\delta V_j} + \partial_j\dot{\delta V_i} - 2\delta_{ij}\dot{\theta}\right] \tag{3.237a}

Setting this to zero:

iδVj˙+jδVi˙=2δijθ˙(3.237b)\partial_i\dot{\delta V_j} + \partial_j\dot{\delta V_i} = 2\delta_{ij}\dot{\theta} \tag{3.237b}

Trace of (3.237b). Contract with δij\delta^{ij}: 2θ˙=6θ˙2\dot{\theta} = 6\dot{\theta}, therefore:

θ˙=0(3.237c)\dot{\theta} = 0 \tag{3.237c}

The velocity divergence is time-independent. Combined with the boundary condition θ0\theta \to 0 at spatial infinity and the constraint 2δVi=iθ\nabla^2\delta V_i = \partial_i\theta from (3.235b): θ\theta is a time-independent harmonic function (2θ=2(2φ)=4φ\nabla^2\theta = \nabla^2(\nabla^2\varphi) = \nabla^4\varphi, which is determined by 2δVi=iθ\nabla^2\delta V_i = \partial_i\theta plus boundary conditions). In vacuum with no sources and decaying boundary conditions: θ=0\theta = 0.

With θ=0\theta = 0, (3.237b) becomes:

iδVj˙+jδVi˙=0(3.237d)\partial_i\dot{\delta V_j} + \partial_j\dot{\delta V_i} = 0 \tag{3.237d}

The velocity perturbation is a Killing field of flat space. (3.237d) says δVi˙\dot{\delta V_i} is a Killing vector: (iδVj)˙=0\partial_{(i}\dot{\delta V_{j)}} = 0. For a perturbation decaying at infinity, the only Killing vectors of flat space that decay are identically zero. Therefore:

δVi˙=0(3.238)\dot{\delta V_i} = 0 \tag{3.238}

The PG velocity perturbation is static. The linearised Einstein equation forces the ether velocity perturbation (in PG form) to be time-independent. This is the static Newtonian potential — not a gravitational wave.

3.14.4 Gravitational Waves Require Departing from Strict PG Form

The result (3.238) means that the PG metric ansatz (unit lapse, flat spatial slices) is too restrictive for radiative solutions. The PG form γij=δij\gamma_{ij} = \delta_{ij} is exact for the stationary Schwarzschild and Kerr solutions but does not accommodate GW, which require oscillating spatial curvature.

In the ether picture, a gravitational wave produces a perturbation of the spatial metric γij=δij+hij\gamma_{ij} = \delta_{ij} + h_{ij} alongside the velocity field. The full metric perturbation around flat space is therefore:

h00=0,h0i=δVi,hij=Hij(3.239)h_{00} = 0, \qquad h_{0i} = -\delta V_i, \qquad h_{ij} = H_{ij} \tag{3.239}

where HijH_{ij} is a small perturbation of the spatial geometry. The ten metric functions are: h00h_{00} (one, zero here), h0ih_{0i} (three, the velocity), and HijH_{ij} (six, symmetric spatial tensor). Total: ten, with h00=0h_{00} = 0 already imposed.

We now derive the constraint and gauge structure that reduces nine functions to two propagating degrees of freedom.

3.14.5 The Lorenz Gauge and Residual Freedom

The trace-reversed perturbation. Define hˉμν=hμν12ημνh\bar{h}_{\mu\nu} = h_{\mu\nu} - \frac{1}{2}\eta_{\mu\nu}h, where h=ημνhμν=(0)/c2+Hii=Hh = \eta^{\mu\nu}h_{\mu\nu} = -(0)/c^2 + H^i{}_i = H, the trace of the spatial perturbation. The linearised Einstein (3.228) in terms of hˉ\bar{h} takes the compact form (the standard trace-reversal identity):

Gμν(1)=12[hˉμν+μαhˉανG^{(1)}_{\mu\nu} = \frac{1}{2}\Big[-\Box\bar{h}_{\mu\nu} + \partial_\mu\partial_\alpha\bar{h}^\alpha{}_\nu +ναhˉαμημναβhˉαβ](3.240)+ \partial_\nu\partial_\alpha\bar{h}^\alpha{}_\mu - \eta_{\mu\nu}\partial_\alpha\partial_\beta\bar{h}^{\alpha\beta}\Big] \tag{3.240}

The Lorenz gauge. Under an infinitesimal coordinate transformation xμxμ+ξμx^\mu \to x^\mu + \xi^\mu:

hμνhμνμξννξμ(3.241)h_{\mu\nu} \to h_{\mu\nu} - \partial_\mu\xi_\nu - \partial_\nu\xi_\mu \tag{3.241}

where ξμ=ημνξν\xi_\mu = \eta_{\mu\nu}\xi^\nu. The trace-reversed perturbation transforms as hˉμνhˉμνμξννξμ+ημναξα\bar{h}_{\mu\nu} \to \bar{h}_{\mu\nu} - \partial_\mu\xi_\nu - \partial_\nu\xi_\mu + \eta_{\mu\nu}\partial_\alpha\xi^\alpha. The divergence transforms as:

μhˉμνμhˉμνξν(3.242)\partial^\mu\bar{h}_{\mu\nu} \to \partial^\mu\bar{h}_{\mu\nu} - \Box\xi_\nu \tag{3.242}

Choosing ξν\xi_\nu to satisfy ξν=μhˉμν\Box\xi_\nu = \partial^\mu\bar{h}_{\mu\nu} (which always has a solution), we can impose the Lorenz gauge condition:

μhˉμν=0(3.243)\partial^\mu\bar{h}_{\mu\nu} = 0 \tag{3.243}

This is four equations (one for each ν\nu), eliminating four of the nine free functions. In Lorenz gauge, (3.240) reduces to:

hˉμν=0(3.244)\Box\bar{h}_{\mu\nu} = 0 \tag{3.244}

Every component of hˉμν\bar{h}_{\mu\nu} satisfies the wave equation. The nine remaining functions (after h00=0h_{00} = 0) minus four Lorenz gauge conditions leaves five.

Residual gauge freedom. The Lorenz condition (3.243) is preserved by any further transformation ξμ\xi^\mu satisfying ξμ=0\Box\xi^\mu = 0. This gives four free functions (one for each component of ξμ\xi^\mu), each satisfying the wave equation. These can be used to impose four additional conditions on hˉμν\bar{h}_{\mu\nu}. Five functions minus four residual gauges leaves one — but this counting overcounts because not all gauge conditions are independent of the Lorenz condition.

The standard counting proceeds as follows from the general structure: starting from ten symmetric components of hμνh_{\mu\nu}, the Lorenz gauge eliminates four, leaving six. Residual gauge freedom (ξμ=0\Box\xi^\mu = 0, four functions) eliminates four more, leaving two. These two are the physical propagating degrees of freedom.

3.14.6 The Transverse-Traceless Gauge

The residual gauge freedom is sufficient to impose the TT gauge conditions:

hˉ0μ=0,hˉii=0,jhˉji=0(3.245)\bar{h}_{0\mu} = 0, \qquad \bar{h}^i{}_i = 0, \qquad \partial_j\bar{h}^{j}{}_i = 0 \tag{3.245}

These are: three conditions from hˉ0i=0\bar{h}_{0i} = 0, one from the trace condition, and three from the divergence condition — but the divergence conditions are not independent of the Lorenz gauge (they are the spatial part of (3.243)), and the hˉ00\bar{h}_{00} condition uses one residual gauge function. The net effect: six components of HijH_{ij}, minus one trace, minus three transverse conditions = two.

Explicit construction. For a plane wave propagating in the zz-direction (kμ=(ω/c,0,0,k)k^\mu = (\omega/c, 0, 0, k) with ω=ck\omega = ck), the TT gauge perturbation has the form:

hijTT=(A+A×0A×A+0000)cos(ωTkz)(3.246)h^{TT}_{ij} = \begin{pmatrix} A_+ & A_\times & 0 \\ A_\times & -A_+ & 0 \\ 0 & 0 & 0 \end{pmatrix} \cos(\omega T - kz) \tag{3.246}

where A+A_+ and A×A_\times are the amplitudes of the plus and cross polarisations respectively. The matrix is traceless (A+A++0=0A_+ - A_+ + 0 = 0), transverse (kjhjxTT=kjhjyTT=0k^j h^{TT}_{jx} = k^j h^{TT}_{jy} = 0 since kk is along zz and hzjTT=0h^{TT}_{zj} = 0), and satisfies hijTT=0\Box h^{TT}_{ij} = 0.

Verification of completeness. These two polarisations exhaust the physical content. Consider the most general symmetric, traceless, transverse 3×33\times 3 matrix for a wave propagating along z^\hat{z}. Tracelessness: hxx+hyy+hzz=0h_{xx} + h_{yy} + h_{zz} = 0. Transversality: hxz=hyz=hzz=0h_{xz} = h_{yz} = h_{zz} = 0. The first two from transversality, combined with tracelessness (hxx+hyy=0h_{xx} + h_{yy} = 0), leave two free components: hxx=hyyh_{xx} = -h_{yy} and hxyh_{xy}. These are A+A_+ and A×A_\times.

3.14.7 The Scalar Breathing Mode Is Non-Radiative

We now prove that the scalar mode identified in Section 3.7 does not radiate.

The scalar mode. In the ether picture, the scalar perturbation is the velocity divergence θ=iδVi=2φ\theta = \partial_i\delta V^i = \nabla^2\varphi, or equivalently the density perturbation δρ\delta\rho (connected to θ\theta by the continuity (3.39)). A breathing mode would be a spherically symmetric oscillation of the spatial metric: Hij=H(T,r)δijH_{ij} = H(T, r)\,\delta_{ij}.

Proof that HδijH\delta_{ij} is non-radiative. Suppose hμνh_{\mu\nu} has only a trace part: hij=Hδijh_{ij} = H\,\delta_{ij}, h0μ=0h_{0\mu} = 0. Then h=3Hh = 3H, hˉij=Hδij12δij3H=12Hδij\bar{h}_{ij} = H\delta_{ij} - \frac{1}{2}\delta_{ij}\cdot 3H = -\frac{1}{2}H\delta_{ij}, and hˉ00=0+c223H=3c2H2\bar{h}_{00} = 0 + \frac{c^2}{2}\cdot 3H = \frac{3c^2H}{2}.

The Lorenz gauge condition (3.243) for ν=0\nu = 0:

μhˉμ0=η00Thˉ00\partial^\mu\bar{h}_{\mu 0} = \eta^{00}\partial_T\bar{h}_{00} =1c2T ⁣(3c2H2)=3H˙2=0(3.247)= -\frac{1}{c^2}\partial_T\!\left(\frac{3c^2H}{2}\right) = -\frac{3\dot{H}}{2} = 0 \tag{3.247}

Therefore H˙=0\dot{H} = 0: the scalar mode is time-independent in Lorenz gauge. A mode that does not oscillate cannot radiate. \square

Physical interpretation. The scalar perturbation HδijH\delta_{ij} represents a uniform expansion or contraction of the spatial geometry. The linearised Einstein equation requires this expansion to be static — it describes a Newtonian-like potential (H=2Φ/c2H = -2\Phi/c^2 in the weak-field limit), not a wave. The constraint H˙=0\dot{H} = 0 is the linearised form of the Hamiltonian constraint: the spatial expansion rate is fixed by the energy density, not by initial data, and it cannot propagate independently.

This resolves the discrepancy with Section 3.7. The wave (3.42) for δρ\delta\rho describes perturbations of the ether density, but the gravitational constraint couples δρ\delta\rho algebraically to the source. The free (vacuum) solution has δρ=0\delta\rho = 0 — the density perturbation does not propagate as a gravitational wave in vacuum. It responds instantaneously to the source distribution, exactly like the Coulomb field in electrodynamics.

3.14.8 The Isaacson Energy Flux

The energy carried by gravitational waves is given by the Isaacson effective stress-energy tensor (Isaacson 1968), which is constructed from the second-order perturbation averaged over several wavelengths:

TμνGW=c432πG ⁣μhijTTνhTTij(3.248)T^{\text{GW}}_{\mu\nu} = \frac{c^4}{32\pi G}\!\left\langle\partial_\mu h^{TT}_{ij}\,\partial_\nu h^{TT\,ij}\right\rangle \tag{3.248}

The energy flux (power per unit area) in the propagation direction z^\hat{z} is:

F=cT0zGWF = -c\,T^{\text{GW}}_{0z} =c332πG ⁣h˙ijTTzhTTij(3.249a)= \frac{c^3}{32\pi G}\!\left\langle\dot{h}^{TT}_{ij}\,\partial_z h^{TT\,ij}\right\rangle \tag{3.249a}

For the plane wave (3.246) with h˙ijTT=ωsin(ωTkz)Aij\dot{h}^{TT}_{ij} = -\omega\sin(\omega T - kz)\cdot A_{ij} and zhijTT=ksin(ωTkz)Aij\partial_z h^{TT}_{ij} = k\sin(\omega T - kz)\cdot A_{ij}, and using sin2=1/2\langle\sin^2\rangle = 1/2:

F=c3ωk32πG12(AijAij)F = \frac{c^3\omega k}{32\pi G}\cdot\frac{1}{2}(A_{ij}A^{ij}) =c2ω232πG(A+2+A×2)(3.249b)= \frac{c^2\omega^2}{32\pi G}(A_+^2 + A_\times^2) \tag{3.249b}

where AijAij=2A+2+2A×2A_{ij}A^{ij} = 2A_+^2 + 2A_\times^2 (the factor of 2 for each polarisation from hxx2+hyy2+2hxy2=2A+2+2A×2h_{xx}^2 + h_{yy}^2 + 2h_{xy}^2 = 2A_+^2 + 2A_\times^2) and ω=ck\omega = ck.

The scalar mode carries no flux. For a pure scalar perturbation hij=H(T,r)δijh_{ij} = H(T,r)\delta_{ij} with H˙=0\dot{H} = 0 (from Section 3.14.7): h˙ij=0\dot{h}_{ij} = 0, so T0zGW=0T^{\text{GW}}_{0z} = 0. The energy flux vanishes identically. The scalar mode does not radiate. \square

The tensor modes carry positive flux. For A+2+A×2>0A_+^2 + A_\times^2 > 0: F>0F > 0. The two TT modes carry energy to infinity. They are the only radiative degrees of freedom.

3.14.9 Gravitational Wave Polarisation Content

Theorem 3.8 (Gravitational wave polarisations).

The ether metric supports exactly two propagating gravitational wave polarisations: plus and cross. The scalar breathing mode identified in Section 3.7 is non-radiative — it is forced to be time-independent by the linearised Einstein equation (Eq 3.247) and carries zero energy flux (Section 3.14.8).

Proof.

By the explicit construction of §Section 3.14.1–3.14.8: the linearised Einstein (3.228), applied to a general perturbation around flat space, reduces in Lorenz gauge (3.243) to the wave (3.244) for nine components. The Lorenz gauge imposes four conditions; residual gauge freedom (ξμ=0\Box\xi^\mu = 0, four functions) imposes four more. The surviving two degrees of freedom are the transverse-traceless modes (3.246): plus and cross polarisations. The scalar (trace) perturbation satisfies H˙=0\dot{H} = 0 in Lorenz gauge (Eq 3.247) and carries zero Isaacson energy flux (Section 3.14.8).

Corollary.

The pure PG perturbation (h0i0h_{0i} \neq 0, hij=0h_{ij} = 0) is entirely non-radiative: the linearised Einstein equation forces δVi˙=0\dot{\delta V_i} = 0 (Eq 3.238). Gravitational waves in the ether manifest as oscillations of the spatial geometry (Hij0H_{ij} \neq 0), physically corresponding to oscillating tidal distortions of the ether medium, not to oscillations of the bulk flow velocity.

3.14.10 Summary of Polarisation Results

The analysis of §Section 3.14.1–3.14.9 establishes that the breathing mode exists as a static (non-radiative) constrained field, analogous to the Coulomb field in electrodynamics. The complete polarisation results are:

(i) Gravitational waves have exactly the GR polarisation content: two tensor modes (++ and ×\times), zero scalar modes, zero vector modes.

(ii) Current LIGO-Virgo-KAGRA observations, which constrain non-GR polarisations [48, 180], are consistent with this prediction.

(iii) At the ether's UV scale e\ell_e, dispersive corrections (Eq 3.46) may modify the polarisation amplitudes. These are suppressed by (fe/c)2(f\ell_e/c)^2 and are undetectable for any foreseeable observatory.

3.15 The Unruh Effect from the Ether

The Hawking effect (Section 3.13) arises from the ether's gravitational horizon — the surface where the ether inflow velocity equals cc. The Unruh effect [181] is the flat-spacetime counterpart: an observer accelerating through the ether's zero-point field detects thermal radiation, even though no horizon exists in the background spacetime.

The Unruh effect is a direct consequence of the ether's ZPF structure (§6) combined with the equivalence principle: an accelerating observer in flat spacetime is locally equivalent to a static observer in a gravitational field, and therefore experiences the ether's quantum fluctuations as thermal. We derive the Unruh temperature from the ether's mode structure without invoking quantum field theory on curved spacetime.

3.15.1 The Rindler Horizon

An observer accelerating uniformly at proper acceleration aa in flat spacetime follows the worldline:

T(τ)=casinh ⁣(aτc)T(\tau) = \frac{c}{a}\sinh\!\left(\frac{a\tau}{c}\right) x(τ)=c2acosh ⁣(aτc)(3.250)x(\tau) = \frac{c^2}{a}\cosh\!\left(\frac{a\tau}{c}\right) \tag{3.250}

where τ\tau is the observer's proper time and the motion is along the xx-axis.

Derivation. The four-acceleration has magnitude aμaμ=a2/c4a^\mu a_\mu = a^2/c^4 (in the convention where aμ=Duμ/dτa^\mu = D u^\mu/d\tau). For motion along xx with uμ=γ(c,v,0,0)u^\mu = \gamma(c, v, 0, 0), the constraint uμuμ=c2u_\mu u^\mu = -c^2 and aμuμ=0a_\mu u^\mu = 0 give dγ/dτ=aγv/c3d\gamma/d\tau = a\gamma v/c^3 and dv/dτ=a/γ3dv/d\tau = a/\gamma^3. With initial conditions v(0)=0v(0) = 0, x(0)=c2/ax(0) = c^2/a: v=ctanh(aτ/c)v = c\tanh(a\tau/c), γ=cosh(aτ/c)\gamma = \cosh(a\tau/c), yielding (3.250) by integration.

The Rindler horizon. The accelerating observer cannot receive signals from the region x<cTx < c\,T (the left Rindler wedge). The boundary x=cTx = c\,T is the Rindler horizon — a null surface in flat spacetime that is causally inaccessible to the accelerating observer.

Connection to the ether picture. In the ether's rest frame, the observer accelerates through the stationary ZPF. From the observer's perspective, the ZPF is Doppler-shifted by the time-varying velocity v(τ)=ctanh(aτ/c)v(\tau) = c\tanh(a\tau/c). The Rindler horizon is the surface from which ZPF modes would need to travel at cc against the observer's acceleration to reach her — the flat-spacetime analog of the acoustic horizon in Section 3.13.

3.15.2 Rindler Coordinates and the Ether Mode Structure

Define Rindler coordinates (η,ρ)(\eta, \rho) adapted to the accelerating observer:

T=ρcsinh ⁣(aηc),x=ρcosh ⁣(aηc)(3.251)T = \frac{\rho}{c}\sinh\!\left(\frac{a\eta}{c}\right), \qquad x = \rho\,\cosh\!\left(\frac{a\eta}{c}\right) \tag{3.251}

where η\eta is the Rindler time (proportional to the observer's proper time at ρ=c2/a\rho = c^2/a: dτ=(aρ/c2)dηd\tau = (a\rho/c^2)\,d\eta) and ρ>0\rho > 0 is the Rindler spatial coordinate. The Minkowski metric in Rindler coordinates is:

ds2=a2ρ2c2dη2+dρ2+dy2+dz2(3.252)ds^2 = -\frac{a^2\rho^2}{c^2}\,d\eta^2 + d\rho^2 + dy^2 + dz^2 \tag{3.252}

Derivation. From (3.251): dT=(ρa/c2)cosh(aη/c)dη+(1/c)sinh(aη/c)dρdT = (\rho a/c^2)\cosh(a\eta/c)\,d\eta + (1/c)\sinh(a\eta/c)\,d\rho and dx=(ρa/c)sinh(aη/c)dη+cosh(aη/c)dρdx = (\rho a/c)\sinh(a\eta/c)\,d\eta + \cosh(a\eta/c)\,d\rho. Computing c2dT2+dx2-c^2dT^2 + dx^2: the dη2d\eta^2 terms give ρ2a2(cosh2+sinh2)/c2=ρ2a2/c2\rho^2a^2(-\cosh^2 + \sinh^2)/c^2 = -\rho^2a^2/c^2; the dρ2d\rho^2 terms give (sinh2+cosh2)=1(-\sinh^2 + \cosh^2) = 1; the cross-terms cancel. This gives (3.252).

The Rindler horizon is at ρ=0\rho = 0. The metric component gηη=a2ρ2/c2g_{\eta\eta} = -a^2\rho^2/c^2 vanishes there, exactly as gTT=(c2v2)g_{TT} = -(c^2 - v^2) vanishes at the ether horizon in Section 3.13 (Eq 3.36). The surface gravity of the Rindler horizon is:

κR=limρ0c22ρgηηgηη1/2\kappa_R = \lim_{\rho \to 0}\frac{c^2}{2}\,\frac{\partial_\rho|g_{\eta\eta}|}{|g_{\eta\eta}|^{1/2}} ×1(gηη)1/2(3.253a)\times \frac{1}{(-g_{\eta\eta})^{1/2}} \tag{3.253a}

More directly: the proper acceleration at Rindler coordinate ρ\rho is alocal=c2/(aρ/c2)1=aa_{\text{local}} = c^2/(a\rho/c^2)^{-1} = a at ρ=c2/a\rho = c^2/a, and the redshift factor between ρ\rho and infinity diverges at ρ=0\rho = 0. The surface gravity, defined as the exponential peeling rate of null rays from the horizon (as in Section 3.13.1), is computed as follows.

Outgoing null rays in Rindler coordinates satisfy ds2=0ds^2 = 0:

dρdη=aρc(3.253b)\frac{d\rho}{d\eta} = \frac{a\rho}{c} \tag{3.253b}

This has the exponential solution ρ(η)=ρ0eaη/c\rho(\eta) = \rho_0\,e^{a\eta/c}, with peeling rate a/ca/c. The surface gravity is:

κR=a(3.253c)\kappa_R = a \tag{3.253c}

This is exact — no approximation to a near-horizon limit is needed, because the Rindler metric (3.252) already has the exact exponential structure everywhere.

3.15.3 Mode Analysis and the Thermal Spectrum

The derivation of the thermal spectrum proceeds identically to Section 3.13.3–3.13.5, with the ether's gravitational horizon replaced by the Rindler horizon.

Retarded time. For outgoing modes, the retarded coordinate is u=η(c/a)lnρu = \eta - (c/a)\ln\rho, obtained by integrating dη=(c/(aρ))dρd\eta = (c/(a\rho))\,d\rho from (3.253b). A mode of Rindler frequency ω\omega has the form:

ψω(η,ρ)=eiωu=eiωηρiωc/a(3.254)\psi_\omega(\eta, \rho) = e^{-i\omega u} = e^{-i\omega\eta}\,\rho^{i\omega c/a} \tag{3.254}

This has the same logarithmic phase singularity at the horizon (ρ0\rho \to 0) as the Hawking mode (3.210) at rrsr \to r_s.

Analytic continuation. The Minkowski vacuum (the ether's ZPF ground state) is defined by positive-frequency modes with respect to the inertial time TT. The Rindler mode (3.254) is positive-frequency with respect to Rindler time η\eta. The two frequency definitions disagree, and the Bogoliubov transformation between them is determined by the analytic continuation of (3.254) across the Rindler horizon, following the identical iϵi\epsilon prescription of Section 3.13.4.

The result — which follows from the identical mathematical structure, with κa\kappa \to a and rrsρr - r_s \to \rho — is:

βω2αω2=e2πωc/a(3.255)\frac{|\beta_\omega|^2}{|\alpha_\omega|^2} = e^{-2\pi\omega c/a} \tag{3.255}

The particle number measured by the accelerating observer:

nω=1e2πωc/a1(3.256)\langle n_\omega \rangle = \frac{1}{e^{2\pi\omega c/a} - 1} \tag{3.256}

This is the Bose–Einstein distribution with temperature:

kBTU=a2πc(3.257)k_B T_U = \frac{\hbar\,a}{2\pi\,c} \tag{3.257}

3.15.4 The Unruh Temperature

Theorem 3.9 (Unruh radiation from the ether).

An observer accelerating uniformly at proper acceleration aa through the ether's zero-point field detects thermal radiation at the Unruh temperature:

TU=a2πkBc(3.258)\boxed{T_U = \frac{\hbar\,a}{2\pi\,k_B\,c}} \tag{3.258}

The radiation has a Planckian spectrum with occupation number nω=(eω/(kBTU)1)1\langle n_\omega \rangle = (e^{\hbar\omega/(k_BT_U)} - 1)^{-1}, where ω\omega is the frequency measured in the accelerating frame.

Proof.

By the construction of §Section 3.15.1–3.15.3: the uniformly accelerating worldline (3.250) defines a Rindler horizon at ρ=0\rho = 0 with surface gravity κR=a\kappa_R = a (Eq 3.253c). The Rindler mode structure (3.254) has the same logarithmic phase singularity as the Hawking mode (3.210). The analytic continuation across the Rindler horizon, by the identical iϵi\epsilon prescription of Section 3.13.4, yields the Bogoliubov coefficient ratio (3.255). The normalisation condition gives the Planckian spectrum (3.256) with temperature (3.257).

Consistency with the Hawking effect. The Hawking temperature (Theorem 3.7) is TH=κ/(2πkBc)T_H = \hbar\kappa/(2\pi k_B c) with κ=c4/(4GM)\kappa = c^4/(4GM). The Unruh temperature is TU=a/(2πkBc)T_U = \hbar a/(2\pi k_B c). The two are related by TU=THT_U = T_H when a=κa = \kappa — that is, when the observer's proper acceleration equals the surface gravity of the black hole. This is the content of the equivalence principle: a static observer hovering at the black hole horizon (with proper acceleration κ\kappa) detects Hawking radiation at temperature TH=κ/(2πkBc)T_H = \hbar\kappa/(2\pi k_Bc), which is precisely the Unruh temperature for that acceleration. In the ether picture, the mechanism is the same in both cases — the observer's acceleration relative to the ZPF produces a thermal spectrum through mode-splitting at the causal horizon.

Numerical evaluation. To detect a temperature of 11 K requires acceleration:

a=2πkBcT=2π×1.381×1023×3×1081.055×1034a = \frac{2\pi\,k_B\,c}{\hbar}\cdot T = \frac{2\pi \times 1.381 \times 10^{-23} \times 3 \times 10^8}{1.055 \times 10^{-34}} =2.47×1020  m/s2(3.259)= 2.47 \times 10^{20}\;\text{m/s}^2 \tag{3.259}

This is approximately 2.5×1019g2.5 \times 10^{19}\,g, far beyond any achievable laboratory acceleration. For the maximum sustained acceleration in current experiments (particle accelerators, 1025\sim 10^{25} m/s2^2 for electrons in a strong laser field): TU40T_U \sim 40 K — measurable in principle but overwhelmed by conventional thermal backgrounds.

3.15.5 Physical Interpretation in the Ether Framework

The Unruh effect has a transparent physical interpretation in the ether picture.

The inertial observer is at rest in the ether (or in uniform motion, which is equivalent by Lorentz invariance). The ether's ZPF (Section 6.1) is the ground state — the state of minimum energy with no real particles. The observer detects no radiation.

The accelerating observer moves with continuously changing velocity relative to the ether. The ZPF modes are Doppler-shifted by this motion: modes approaching from ahead are blueshifted, modes from behind are redshifted. For uniform acceleration, the cumulative Doppler shift over the observer's history produces a precise Planckian distribution — not because the ZPF has been heated, but because the accelerating observer's definition of "positive frequency" (and hence "particle") differs from the inertial definition.

The Rindler horizon is the surface behind the accelerating observer from which ZPF modes cannot catch up — they are redshifted to zero frequency before they arrive. This creates the same mode-splitting as the ether's gravitational horizon in Section 3.13: ZPF fluctuations near the Rindler horizon are torn apart by the observer's acceleration, with one component escaping forward (detected as a thermal particle) and the other falling behind the horizon.

The energy source. The detected radiation carries energy. Where does it come from? The observer must be accelerated by an external force (a rocket, an electric field). The work done by this force against the radiation reaction of the emitted particles provides the energy. In the ether picture: the accelerating observer disturbs the ZPF, converting virtual fluctuations into real excitations, with the energy supplied by whatever agent maintains the acceleration.

3.16 Ether Conservation and the Sink Problem Resolved

Section 3.9.2 noted an apparent paradox: the Schwarzschild ether flow (Eq 3.22) has nonzero divergence (Eq 3.57), so the Newtonian continuity equation tρe+(ρeV)=0\partial_t\rho_e + \nabla\cdot(\rho_e\mathbf{V}) = 0 is not satisfied for constant ether density ρe=ρ0\rho_e = \rho_0. Three possible resolutions were discussed — mass as ether sink, compressible ether, and effective description.

Theorem 3.5 resolves this problem. The ether's field equation is the Einstein equation, and the Einstein equation implies covariant energy-momentum conservation: μTμν=0\nabla_\mu T^{\mu\nu} = 0 (the contracted Bianchi identity). The ether IS conserved — but the relevant conservation law is the covariant one, not the Newtonian one. The Newtonian continuity equation is the leading-order approximation to μTμ0=0\nabla_\mu T^{\mu 0} = 0; at post-Newtonian order, additional terms enter that account for the gravitational field's energy and momentum. This section derives these terms explicitly.

3.16.1 The Covariant Conservation Law

The stress-energy tensor of a perfect fluid with four-velocity UμU^\mu, energy density ε\varepsilon, and pressure PP is:

Tμν=(ε+P/c2)UμUν+Pgμν(3.260)T^{\mu\nu} = (\varepsilon + P/c^2)\,U^\mu U^\nu + P\,g^{\mu\nu} \tag{3.260}

For the pressureless (P=0P = 0) ether condensate in its normal phase:

Tμν=εUμUν(3.261)T^{\mu\nu} = \varepsilon\,U^\mu U^\nu \tag{3.261}

The covariant conservation law μTμν=0\nabla_\mu T^{\mu\nu} = 0 expands to:

μ(εUμUν)=Uνμ(εUμ)+εUμμUν=0(3.262)\nabla_\mu(\varepsilon\,U^\mu U^\nu) = U^\nu\nabla_\mu(\varepsilon\,U^\mu) + \varepsilon\,U^\mu\nabla_\mu U^\nu = 0 \tag{3.262}

Projecting along UνU^\nu (energy conservation) and orthogonal to UνU^\nu (momentum conservation):

μ(εUμ)=0(3.263)\nabla_\mu(\varepsilon\,U^\mu) = 0 \tag{3.263} εUμμUν=0(geodesic equation)(3.264)\varepsilon\,U^\mu\nabla_\mu U^\nu = 0 \qquad (\text{geodesic equation}) \tag{3.264}

(3.263) is the covariant continuity equation — the relativistic generalisation of tρ+(ρV)=0\partial_t\rho + \nabla\cdot(\rho\mathbf{V}) = 0.

3.16.2 Covariant Continuity in PG Coordinates

In PG coordinates, the ether four-velocity for a freely falling fluid element is Uμ=nμc=(1,Vi)U^\mu = n^\mu c = (1, -V^i) (from Eq 3.96, with the normalisation UμUμ=c2U_\mu U^\mu = -c^2, and using the fact that freely falling ether elements have four-velocity proportional to the unit normal). More precisely, U0=cn0=1U^0 = c\,n^0 = 1 and Ui=cni=ViU^i = c\,n^i = -V^i.

Verification of normalisation. UμUμ=gμνUμUνU_\mu U^\mu = g_{\mu\nu}U^\mu U^\nu. With U0=1U^0 = 1, Ui=ViU^i = -V^i:

UμUμ=g00(U0)2+2g0iU0Ui+gijUiUjU_\mu U^\mu = g_{00}(U^0)^2 + 2g_{0i}U^0 U^i + g_{ij}U^i U^j =(c2V2)+2Vi(Vi)+δijViVj= -(c^2 - V^2) + 2V_i(-V^i) + \delta_{ij}V^iV^j =c2+V22V2+V2=c2(3.265)= -c^2 + V^2 - 2V^2 + V^2 = -c^2 \tag{3.265}

The covariant divergence of εUμ\varepsilon\,U^\mu is:

μ(εUμ)=1gμ ⁣(g  εUμ)(3.266)\nabla_\mu(\varepsilon\,U^\mu) = \frac{1}{\sqrt{-g}}\,\partial_\mu\!\left(\sqrt{-g}\;\varepsilon\,U^\mu\right) \tag{3.266}

From Section 3.11.1: g=c\sqrt{-g} = c (constant, Eq 3.93). Therefore:

μ(εUμ)=1cμ ⁣(cεUμ)\nabla_\mu(\varepsilon\,U^\mu) = \frac{1}{c}\,\partial_\mu\!\left(c\,\varepsilon\,U^\mu\right) =μ(εUμ)(3.267)= \partial_\mu(\varepsilon\,U^\mu) \tag{3.267}

The constant determinant eliminates the Christoffel-symbol terms entirely. Expanding:

T(εU0)+i(εUi)=Tε+i(ε(Vi))\partial_T(\varepsilon\,U^0) + \partial_i(\varepsilon\,U^i) = \partial_T\varepsilon + \partial_i(\varepsilon\,(-V^i)) =Tεi(εVi)=0(3.268)= \partial_T\varepsilon - \partial_i(\varepsilon\,V^i) = 0 \tag{3.268}

This is:

εT(εV)=0(3.269)\frac{\partial\varepsilon}{\partial T} - \nabla\cdot(\varepsilon\,\mathbf{V}) = 0 \tag{3.269}

Note the minus sign in front of the divergence. This arises because the ether flows inward (V\mathbf{V} points toward the mass) while Ui=ViU^i = -V^i points outward in the coordinate sense. The sign is consistent: the ether flows inward, so the flux εV\varepsilon\mathbf{V} points inward, and (εV)-\nabla\cdot(\varepsilon\mathbf{V}) is positive near the mass, compensating the accumulation of ether.

Comparison with the Newtonian continuity equation. The standard form tρ+(ρv)=0\partial_t\rho + \nabla\cdot(\rho\mathbf{v}) = 0 has a plus sign because v\mathbf{v} is the fluid velocity in the direction of motion. In PG coordinates, V\mathbf{V} is defined as the shift vector (pointing inward, Vi>0V^i > 0 for inward radial flow), and the four-velocity has Ui=ViU^i = -V^i. With the identification ε=ρ0c2\varepsilon = \rho_0 c^2 (constant energy density):

(ρ0c2V)=0    V=0(3.270)-\nabla\cdot(\rho_0 c^2\,\mathbf{V}) = 0 \implies \nabla\cdot\mathbf{V} = 0 \tag{3.270}

But from Eq (3.57): V0\nabla\cdot\mathbf{V} \neq 0 for the Schwarzschild flow. So either ε\varepsilon is not constant, or (3.269) is not the complete equation. We now show it is the latter.

3.16.3 The Resolution: Relativistic Mass-Energy

The key is that ε\varepsilon in the covariant conservation law (3.263) is the energy density measured by a comoving observer — the proper energy density. For a freely falling ether element, this includes the rest-mass energy AND the kinetic energy of the fall:

ε(r)=ρ0c2+12ρ0V2+O(V4/c2)(3.271)\varepsilon(r) = \rho_0 c^2 + \frac{1}{2}\rho_0 V^2 + O(V^4/c^2) \tag{3.271}

The kinetic energy density 12ρ0V2\frac{1}{2}\rho_0 V^2 is a post-Newtonian correction that modifies the conservation law.

However, a more precise treatment uses the ADM energy density. The Eulerian energy density is ρE=Tμνnμnν\rho_E = T_{\mu\nu}\,n^\mu n^\nu, which for a pressureless fluid with four-velocity UμU^\mu is:

ρE=ε(Uμnμ)2/c2(3.272)\rho_E = \varepsilon\,(U_\mu n^\mu)^2/c^2 \tag{3.272}

Computing UμnμU_\mu n^\mu: Uμnμ=gμνUνnμU_\mu n^\mu = g_{\mu\nu}U^\nu n^\mu. With Uν=(1,Vi)U^\nu = (1, -V^i) and nμ=(1/c,Vi/c)n^\mu = (1/c, -V^i/c):

Uμnμ=g0011c+g0i ⁣(1Vic+(Vi)1c)+gij(Vi)VjcU_\mu n^\mu = g_{00}\cdot 1 \cdot\frac{1}{c} + g_{0i}\!\left(1\cdot\frac{-V^i}{c} + (-V^i)\cdot\frac{1}{c}\right) + g_{ij}(-V^i)\frac{-V^j}{c} =(c2V2)c+Vi2Vic+V2c= \frac{-(c^2-V^2)}{c} + V_i\frac{-2V^i}{c} + \frac{V^2}{c} =c2+V2c2V2c+V2c=c(3.273)= \frac{-c^2+V^2}{c} - \frac{2V^2}{c} + \frac{V^2}{c} = -c \tag{3.273}

Therefore ρE=εc2/c2=ε\rho_E = \varepsilon\,c^2/c^2 = \varepsilon. For a freely falling pressureless fluid in PG coordinates, the Eulerian and proper energy densities coincide.

The proper resolution comes from examining what (3.269) actually requires when applied to the exact Schwarzschild solution.

3.16.4 Exact Evaluation for Schwarzschild

For the Schwarzschild flow: Vi=2GMxi/r3/2V^i = -\sqrt{2GM}\,x^i/r^{3/2} (inward, so ViV^i as defined in Eq 3.22 has the radial component Vr=2GM/rV_r = -\sqrt{2GM/r} negative — but in the ADM convention used in Section 3.11 and throughout this section, ViV^i is the shift vector with Vr>0V^r > 0 for inward flow). We must be careful with signs.

In spherical coordinates with the convention V=Vr(r)r^\mathbf{V} = V_r(r)\,\hat{\mathbf{r}} where Vr>0V_r > 0 denotes inward flow (consistent with the PG metric cross-term gTr=Vr<0g_{Tr} = -V_r < 0):

Vr=2GMr(3.274)V_r = \sqrt{\frac{2GM}{r}} \tag{3.274}

The divergence is:

V=1r2ddr(r2Vr)=1r2ddr ⁣(r22GMr)=1r2ddr ⁣(2GMr3/2)\nabla\cdot\mathbf{V} = \frac{1}{r^2}\frac{d}{dr}(r^2 V_r) = \frac{1}{r^2}\frac{d}{dr}\!\left(r^2\sqrt{\frac{2GM}{r}}\right) = \frac{1}{r^2}\frac{d}{dr}\!\left(\sqrt{2GM}\,r^{3/2}\right) =2GMr232r1/2=322GMr3(3.275)= \frac{\sqrt{2GM}}{r^2}\cdot\frac{3}{2}r^{1/2} = \frac{3}{2}\sqrt{\frac{2GM}{r^3}} \tag{3.275}

This is positive: the ether flow diverges (spreads out) as it accelerates inward through successively smaller spheres — the velocity increases faster (r1/2\propto r^{-1/2}) than the area decreases (r2\propto r^{-2}).

The Newtonian continuity equation with constant ρ0\rho_0 requires V=0\nabla\cdot\mathbf{V} = 0. (3.275) shows V0\nabla\cdot\mathbf{V} \neq 0. This is the apparent paradox of Section 3.9.2.

The covariant conservation law (3.269) requires Tε=(εV)\partial_T\varepsilon = \nabla\cdot(\varepsilon\mathbf{V}) for a static configuration (Tε=0\partial_T\varepsilon = 0). This gives (εV)=0\nabla\cdot(\varepsilon\mathbf{V}) = 0, which is satisfied if:

ε(r)Vr(r)r2=const(3.276)\varepsilon(r)\,V_r(r)\,r^2 = \text{const} \tag{3.276}

From (3.274): Vrr2=2GMr3/2V_r\,r^2 = \sqrt{2GM}\,r^{3/2}. For (3.276) to hold:

ε(r)=C2GMr3/2(3.277)\varepsilon(r) = \frac{C}{\sqrt{2GM}\,r^{3/2}} \tag{3.277}

for some constant CC. The energy density must decrease as r3/2r^{-3/2} — the ether is compressed near the mass.

Physical interpretation. The constant-density assumption (ε=ρ0c2\varepsilon = \rho_0 c^2) that underlies Theorem 3.2 is an approximation. The exact solution of the covariant conservation law has εr3/2\varepsilon \propto r^{-3/2}. This density variation modifies the conformal factor in the ether metric (Eq 3.17) from a constant to ρe(r)/c\rho_e(r)/c, introducing a position-dependent correction.

3.16.5 The Magnitude of the Correction

The density variation (3.277) is a post-Newtonian effect. To see this, normalise ε\varepsilon so that ερ0c2\varepsilon \to \rho_0 c^2 as rr \to \infty. The conservation law εVrr2=const\varepsilon V_r r^2 = \text{const} requires:

ε(r)=ρ0c2Vr()r2Vr(r)r2(3.278)\varepsilon(r) = \rho_0 c^2 \cdot \frac{V_r(\infty)\,r_\infty^2}{V_r(r)\,r^2} \tag{3.278}

As rr \to \infty: Vr0V_r \to 0 and the product Vrr22GMr3/2V_r\,r^2 \to \sqrt{2GM}\,r^{3/2} \to \infty. The flux at infinity is not finite for the Schwarzschild profile — reflecting the fact that the Schwarzschild solution describes an eternal black hole with ether flowing in from infinity, not a realistic astrophysical configuration.

For a more physical setup, consider the ether flowing through a shell between radii r1r_1 and r2>r1r_2 > r_1. The mass flux through a sphere of radius rr is:

M˙e(r)=4πr2ρe(r)Vr(r)(3.279)\dot{M}_e(r) = 4\pi r^2\,\rho_e(r)\,V_r(r) \tag{3.279}

Conservation of mass flux (M˙e\dot{M}_e independent of rr) gives:

ρe(r)=M˙e4πr2Vr(r)=M˙e4π2GMr3/2(3.280)\rho_e(r) = \frac{\dot{M}_e}{4\pi r^2 V_r(r)} = \frac{\dot{M}_e}{4\pi\sqrt{2GM}\,r^{3/2}} \tag{3.280}

The fractional density deviation from ρ0\rho_0 at radius rr is:

δρeρ0=ρe(r)ρ0ρ0(3.281)\frac{\delta\rho_e}{\rho_0} = \frac{\rho_e(r) - \rho_0}{\rho_0} \tag{3.281}

For the regime where the density variation is small (δρe/ρ01|\delta\rho_e/\rho_0| \ll 1), the mass flux is approximately M˙e4πr2ρ0Vr\dot{M}_e \approx 4\pi r^2\rho_0 V_r, and (3.280) gives ρeρ0\rho_e \approx \rho_0 (self-consistent). The correction appears at the next order.

The post-Newtonian expansion. Write ε=ρ0c2(1+δ)\varepsilon = \rho_0 c^2(1 + \delta) with δ1|\delta| \ll 1. The covariant conservation (3.269) in steady state:

(εV)=εV+Vε=0(3.282)\nabla\cdot(\varepsilon\mathbf{V}) = \varepsilon\,\nabla\cdot\mathbf{V} + \mathbf{V}\cdot\nabla\varepsilon = 0 \tag{3.282} ρ0c2(1+δ)V+ρ0c2Vrdδdr=0(3.283)\rho_0 c^2(1+\delta)\,\nabla\cdot\mathbf{V} + \rho_0 c^2\,V_r\,\frac{d\delta}{dr} = 0 \tag{3.283}

At leading order (δ1\delta \ll 1):

V+Vrdδdr=0(3.284)\nabla\cdot\mathbf{V} + V_r\frac{d\delta}{dr} = 0 \tag{3.284}

Using (3.275): V=32GM/(2r3/2)\nabla\cdot\mathbf{V} = 3\sqrt{2GM}/(2r^{3/2}). The velocity gradient term: Vrdδ/dr=2GM/rδ(r)V_r\,d\delta/dr = \sqrt{2GM/r}\,\delta'(r). Therefore:

2GMrδ(r)=32GM2r3/2(3.285)\sqrt{\frac{2GM}{r}}\,\delta'(r) = -\frac{3\sqrt{2GM}}{2r^{3/2}} \tag{3.285} δ(r)=32r(3.286)\delta'(r) = -\frac{3}{2r} \tag{3.286} δ(r)=32ln ⁣(rr)(3.287)\delta(r) = -\frac{3}{2}\ln\!\left(\frac{r}{r_\infty}\right) \tag{3.287}

where rr_\infty is the reference radius at which δ=0\delta = 0 (i.e., ε=ρ0c2\varepsilon = \rho_0 c^2).

This logarithmic divergence signals the breakdown of the small-δ\delta approximation at rre2/3r \sim r_\infty e^{-2/3}. But for the physically relevant regime rrsr \gg r_s:

δ(r)=32ln ⁣(rr)(3.288)|\delta(r)| = \frac{3}{2}\left|\ln\!\left(\frac{r}{r_\infty}\right)\right| \tag{3.288}

The density correction is logarithmic, not polynomial, in rr — it grows slowly and remains small over many decades of radius.

Effect on the metric. The conformal factor in the ether metric (Eq 3.17) becomes ρe(r)/c=ρ0(1+δ)/c\rho_e(r)/c = \rho_0(1+\delta)/c. This introduces a position-dependent conformal rescaling:

gμνcorrected=(1+δ(r))gμνPG(3.289)g_{\mu\nu}^{\text{corrected}} = (1 + \delta(r))\,g_{\mu\nu}^{\text{PG}} \tag{3.289}

For null geodesics (light paths, gravitational redshift, horizon locations), a static conformal factor does not alter the predictions — null geodesics are conformally invariant (Section 3.3, Remark on the conformal factor). For timelike geodesics (massive particle orbits), the correction introduces a fractional deviation:

δaaNδ32ln(r/r)(3.290)\frac{\delta a}{a_N} \sim \delta \sim \frac{3}{2}\ln(r/r_\infty) \tag{3.290}

This is parametrically of order ln(r/rs)\ln(r/r_s) — a logarithmic post-Newtonian correction.

Relation to the field equation. The density variation (3.287) arises from exact covariant conservation (μTμν=0\nabla_\mu T^{\mu\nu} = 0, guaranteed by the Bianchi identity and Theorem 3.5), not from an arbitrary gauge transformation. The constant-density PG metric solves the Einstein equation exactly; the density correction (3.289) is the leading post-Newtonian correction that maintains covariant conservation, and is therefore consistent with the Einstein equation at all orders.

3.16.6 Resolution of the Three Interpretations

We now revisit the three interpretations offered in Section 3.9.2.

(a) Mass as ether sink. In the covariant formulation, the ether IS conserved: μ(εUμ)=0\nabla_\mu(\varepsilon U^\mu) = 0 (Eq 3.263). There is no sink. The apparent non-conservation arises from using the Newtonian continuity equation (which ignores relativistic corrections) with a constant density (which ignores the compressibility required by the exact conservation law). The "sink" interpretation is an artifact of an inconsistent approximation.

(b) Compressible ether. Correct. The exact conservation law requires ε(r)1/(r2Vr)r3/2\varepsilon(r) \propto 1/(r^2 V_r) \propto r^{-3/2}. The ether is compressible, and the density variation is a post-Newtonian effect. This does not conflict with Theorem 3.2: the constant-density assumption yields the Schwarzschild metric up to a constant conformal factor, and the density correction (3.289) is a higher-order conformal correction that does not affect the leading-order predictions.

(c) Effective description. Also correct, in the sense that the constant-density PG metric is the leading-order effective description. The density correction (3.287) is the first post-Newtonian correction to this effective description. For all weak-field applications (solar system tests, galaxy dynamics, gravitational waves), the correction is negligible.

The definitive resolution: The ether is conserved in the relativistic sense (μTμν=0\nabla_\mu T^{\mu\nu} = 0, guaranteed by the Bianchi identity and Theorem 3.5). The constant-density assumption is an approximation valid at leading post-Newtonian order, with logarithmic corrections at the next order. No ether is created, destroyed, or absorbed. The "sink problem" of Section 3.9.2 is resolved.

3.16.7 Comparison with Standard GR

In standard GR, the analogous question does not arise because there is no "medium" whose density could vary. The stress-energy tensor of matter satisfies μTmatterμν=0\nabla_\mu T^{\mu\nu}_{\text{matter}} = 0, which determines the matter's motion (geodesic equation for dust). The gravitational field carries energy described by the Landau–Lifshitz pseudotensor, but this energy is not localisable — its integral over a region depends on the choice of coordinates [182].

In the ether framework, the gravitational field energy is localisable: it is the kinetic energy 12ρeV2\frac{1}{2}\rho_e V^2 of the ether flow (Section 3.11.5). The total energy — ether rest mass plus kinetic energy — is exactly conserved by the covariant conservation law. This is an interpretive advantage of the ether framework: the energy of the gravitational field has a concrete, localisable meaning in the ether rest frame as the kinetic energy of a physical medium, unlike the non-localisable pseudotensor energy of standard GR.

3.17 The Einstein Equation from Ether Thermodynamics

Section 3.11 derived the Einstein equation from the ether metric via the Weinberg–Deser–Lovelock uniqueness theorems (Theorem 3.5). The derivation takes the Newtonian limit as its single empirical input and uses uniqueness to fix the nonlinear extension. We now present an independent second derivation that proceeds from the thermodynamic properties of the ether's zero-point field, following the route pioneered by Jacobson [183]. The two derivations use different physical assumptions and arrive at the same result — the Einstein equation — providing strong mutual corroboration.

The Jacobson route does not use the Newtonian limit as an input. Its inputs are: (i) the ether supports a zero-point field whose entanglement entropy across any horizon is proportional to the horizon area (derived from mode counting in Section 3.17.2); (ii) the Unruh effect holds for the acoustic metric (established in Theorem 3.9, Section 3.15); (iii) the ether is in local thermodynamic equilibrium (a natural assumption for a superfluid at scales much larger than the healing length). The Einstein equation — including the Newtonian limit — is an output.

3.17.1 The Physical Ingredients

The derivation requires three results already established in this monograph:

(i) The acoustic metric (Theorem 3.1, Section 3.1). The ether's perturbations propagate on the effective Lorentzian metric gμνg_{\mu\nu} determined by the ether's flow velocity and sound speed. This metric defines causal structure, horizons, and geodesics.

(ii) The Unruh effect (Theorem 3.9, Section 3.15). An observer accelerating uniformly at proper acceleration aa through the ether detects thermal radiation at temperature TU=a/(2πkBc)T_U = \hbar a/(2\pi k_B c). Equivalently, any local Rindler horizon in the ether metric has a temperature:

T=κ2πkBc(3.291)T = \frac{\hbar\kappa}{2\pi k_B c} \tag{3.291}

where κ\kappa is the surface gravity of the horizon.

(iii) The ether's zero-point field (Section 6.1, Theorem 4.2). The ether supports electromagnetic and phononic quantum fluctuations whose spectral density is uniquely determined by Lorentz invariance.

To these we add one new ingredient:

(iv) The entanglement entropy of the ZPF across a horizon is proportional to the horizon area. We derive this in Section 3.17.2.

3.17.2 Entanglement Entropy from ZPF Mode Counting

Consider a Rindler horizon H\mathcal{H} — a null surface in the ether metric that divides space into two causally disconnected regions. The ether's ZPF modes span both regions. Tracing over the modes in the causally inaccessible region produces an entanglement entropy for the accessible region.

The mode-counting argument. A free scalar field ϕ\phi on a (3+1)(3+1)-dimensional spacetime, restricted to modes with wavelength λ>UV\lambda > \ell_{\text{UV}} (the UV cutoff), has entanglement entropy across a smooth surface of area AA given by [184, 185]:

Sent=NkBA48πUV2+sub-leading terms(3.292)S_{\text{ent}} = \frac{\mathcal{N}\,k_B\,A}{48\pi\,\ell_{\text{UV}}^2} + \text{sub-leading terms} \tag{3.292}

where N\mathcal{N} is the number of field species contributing to the entropy. This result was derived by Bombelli, Koul, Lee, and Sorkin [184] and independently by Srednicki [185] using the replica trick and lattice regularisation. The area scaling is universal — it depends only on the dimensionality of spacetime and the UV cutoff, not on the details of the field theory.

Derivation sketch. The entanglement entropy is computed by:

(a) Discretising the field ϕ\phi on a spatial lattice with spacing UV\ell_{\text{UV}}.

(b) Computing the ground-state density matrix ρ^\hat{\rho} of the full system.

(c) Tracing over lattice sites on one side of the surface: ρ^red=Troutsideρ^\hat{\rho}_{\text{red}} = \text{Tr}_{\text{outside}}\hat{\rho}.

(d) Computing S=kBTr(ρ^redlnρ^red)S = -k_B\,\text{Tr}(\hat{\rho}_{\text{red}}\ln\hat{\rho}_{\text{red}}).

For a free field, ρ^\hat{\rho} is Gaussian, and the entropy is determined by the two-point correlator restricted to the surface. The leading term is proportional to the number of lattice sites on the surface, which scales as A/UV2A/\ell_{\text{UV}}^2. The coefficient 1/(48π)1/(48\pi) was computed by Srednicki [185] for a minimally coupled scalar field via numerical lattice diagonalisation and confirmed analytically by Solodukhin [186].

Application to the ether. In the ether framework, the UV cutoff is the transverse microstructure scale e\ell_e (for electromagnetic modes) or the healing length ξ\xi (for phononic modes). The number of contributing species N\mathcal{N} counts the electromagnetic polarisations (2) and the phonon mode (1), giving N=3\mathcal{N} = 3 at minimum. Additional species (from multi-component ether structure required by Proposition 6.1) increase N\mathcal{N}.

Writing the entanglement entropy as:

Sent=ηA(3.293)S_{\text{ent}} = \eta\,A \tag{3.293}

where η\eta is the entropy per unit area:

η=NkB48πe2(3.294)\eta = \frac{\mathcal{N}\,k_B}{48\pi\,\ell_e^2} \tag{3.294}

For later convenience, we define η\eta in terms of a length scale grav\ell_{\text{grav}} by:

η=kB4grav2(3.295)\eta = \frac{k_B}{4\,\ell_{\text{grav}}^2} \tag{3.295}

so that S=kBA/(4grav2)S = k_B A/(4\ell_{\text{grav}}^2), matching the Bekenstein–Hawking form. The gravitational length scale is:

grav2=12πe2N(3.296)\ell_{\text{grav}}^2 = \frac{12\pi\,\ell_e^2}{\mathcal{N}} \tag{3.296}

We will show that grav\ell_{\text{grav}} is identified with the Planck length P=G/c3\ell_P = \sqrt{\hbar G/c^3}, from which Newton's constant GG is determined.

3.17.3 Local Rindler Horizons in the Ether

At any point pp in the ether spacetime, we can construct a local Rindler horizon by considering an observer accelerating with proper acceleration aa through the ether. In the observer's frame, the ether flows past with increasing velocity, and a causal horizon exists at a proper distance c2/ac^2/a behind the observer (Section 3.15.1).

The local construction. Choose a point pp and a future-directed null vector kμk^\mu at pp. The null geodesic through pp with tangent kμk^\mu generates a small patch of a null surface H\mathcal{H}. We parametrise this surface by affine parameter λ\lambda, with λ=0\lambda = 0 at pp and kμ=dxμ/dλk^\mu = dx^\mu/d\lambda.

The approximate boost Killing vector in the neighbourhood of pp is:

χμ=κc2λkμ(3.297)\chi^\mu = \frac{\kappa}{c^2}\,\lambda\,k^\mu \tag{3.297}

where κ\kappa is the surface gravity (with dimensions of acceleration, as in Eqs. 3.195 and 3.253c) and λ\lambda is the affine parameter (with dimensions of length). The factor c2c^2 converts from the physical surface gravity κ\kappa [m/s2^2] to the geometric surface gravity κ/c2\kappa/c^2 [m1^{-1}], ensuring χμ\chi^\mu is dimensionless. This satisfies χμλ=0=0\chi^\mu|_{\lambda=0} = 0 (the Killing vector vanishes at the bifurcation point) and μχνλ=0=(κ/c2)(kμnνkνnμ)\nabla_\mu\chi_\nu|_{\lambda=0} = (\kappa/c^2)\,(k_\mu n_\nu - k_\nu n_\mu) where nμn^\mu is an auxiliary null vector normalised as kμnμ=1k_\mu n^\mu = -1.

In the ether framework, the local Rindler horizon is a local acoustic horizon: the surface where the ether flow velocity relative to the accelerating observer equals the local sound speed (or light speed, for electromagnetic perturbations). The Unruh temperature associated with this horizon is ((3.291)):

T=κ2πkBc(3.298)T = \frac{\hbar\kappa}{2\pi k_B c} \tag{3.298}

3.17.4 The Energy Flux Through the Horizon

The energy flux through the horizon patch is computed by contracting the matter stress-energy tensor with the approximate boost Killing vector and integrating over the horizon surface.

The surface element. The null surface H\mathcal{H} has surface element dΣμ=kμdAdλd\Sigma^\mu = k^\mu\,dA\,d\lambda, where dAdA is the cross-sectional area element of the pencil of generators at affine parameter λ\lambda.

The energy flux. The heat absorbed by the horizon (the energy flowing through H\mathcal{H} as seen by the accelerating observer) is:

δQ=HTμνχμdΣν(3.299)\delta Q = -\int_{\mathcal{H}} T_{\mu\nu}\,\chi^\mu\,d\Sigma^\nu \tag{3.299}

The minus sign follows the thermodynamic convention: positive δQ\delta Q corresponds to energy entering the system (the horizon).

Substituting χμ=(κ/c2)λkμ\chi^\mu = (\kappa/c^2)\lambda k^\mu and dΣν=kνdAdλd\Sigma^\nu = k^\nu dA\,d\lambda:

δQ=Tμνκc2λkμkνdAdλ\delta Q = -\int T_{\mu\nu}\,\frac{\kappa}{c^2}\lambda k^\mu\,k^\nu\,dA\,d\lambda =κc2TμνkμkνλdAdλ(3.300)= -\frac{\kappa}{c^2}\int T_{\mu\nu}\,k^\mu k^\nu\,\lambda\,dA\,d\lambda \tag{3.300}

For matter satisfying the null energy condition (Tμνkμkν0T_{\mu\nu}k^\mu k^\nu \geq 0), the integrand is non-negative. With λ>0\lambda > 0 (past the bifurcation point, in the future direction) and κ>0\kappa > 0, the integral is positive. The minus sign ensures δQ>0\delta Q > 0: energy flowing through the horizon heats the system.

3.17.5 The Area Change from the Raychaudhuri Equation

The cross-sectional area of the pencil of null generators evolves according to the Raychaudhuri equation for a null geodesic congruence [165, 187]:

dθdλ=12θ2σμνσμνRμνkμkν(3.301)\frac{d\theta}{d\lambda} = -\frac{1}{2}\theta^2 - \sigma_{\mu\nu}\sigma^{\mu\nu} - R_{\mu\nu}\,k^\mu k^\nu \tag{3.301}

where θ=μkμ\theta = \nabla_\mu k^\mu is the expansion scalar and σμν\sigma_{\mu\nu} is the shear tensor of the congruence.

Near-bifurcation expansion. At the bifurcation point λ=0\lambda = 0, the generators of the local Rindler horizon have:

θ(λ=0)=0,σμν(λ=0)=0(3.302)\theta(\lambda=0) = 0, \qquad \sigma_{\mu\nu}(\lambda=0) = 0 \tag{3.302}

(The expansion and shear vanish at the bifurcation point of any Killing horizon, by the properties of the boost Killing vector [165].)

To leading order in λ\lambda, (3.301) gives:

dθdλλ=0=Rμνkμkν(3.303)\frac{d\theta}{d\lambda}\bigg|_{\lambda=0} = -R_{\mu\nu}\,k^\mu k^\nu \tag{3.303}

Integrating:

θ(λ)=Rμνkμkνλ+O(λ2)(3.304)\theta(\lambda) = -R_{\mu\nu}\,k^\mu k^\nu\,\lambda + O(\lambda^2) \tag{3.304}

The area change. The fractional rate of change of the cross-sectional area is d(lnA)/dλ=θd(\ln A)/d\lambda = \theta. For the pencil of generators from λ=0\lambda = 0 to some small λ0\lambda_0:

δA=0λ0 ⁣θdAdλ=RμνkμkνλdAdλ+O(λ02)(3.305)\delta A = \int_0^{\lambda_0}\!\int \theta\,dA\,d\lambda = -\int R_{\mu\nu}\,k^\mu k^\nu\,\lambda\,dA\,d\lambda + O(\lambda_0^2) \tag{3.305}

The entropy change associated with this area change is (using (3.293)):

δS=ηδA=ηRμνkμkνλdAdλ(3.306)\delta S = \eta\,\delta A = -\eta\int R_{\mu\nu}\,k^\mu k^\nu\,\lambda\,dA\,d\lambda \tag{3.306}

3.17.6 The Clausius Relation and the Field Equation

The Clausius relation. For a system in local thermodynamic equilibrium at temperature TT, the entropy change produced by a reversible heat flux δQ\delta Q is:

δQ=TδS(3.307)\delta Q = T\,\delta S \tag{3.307}

In the ether framework, this relation is the local equilibrium condition for the ether at each spacetime point. The temperature is the Unruh temperature (3.298), the entropy is the ZPF entanglement entropy (3.293), and the heat is the energy flux through the local horizon (3.300).

Substitution. Substituting (3.300), (3.298), and (3.306) into (3.307):

κc2TμνkμkνλdAdλ=κ2πkBc(ηRμνkμkνλdAdλ)(3.308)-\frac{\kappa}{c^2}\int T_{\mu\nu}\,k^\mu k^\nu\,\lambda\,dA\,d\lambda = \frac{\hbar\kappa}{2\pi k_B c}\cdot\left(-\eta\int R_{\mu\nu}\,k^\mu k^\nu\,\lambda\,dA\,d\lambda\right) \tag{3.308}

Cancellation. The factors κ\kappa, λ\lambda, dAdA, and dλd\lambda appear identically on both sides and cancel. The minus signs cancel. The factor 1/c21/c^2 on the left combines with 1/c1/c in the Unruh temperature on the right:

1c2Tμνkμkν=η2πkBc  Rμνkμkν(3.309a)\frac{1}{c^2}\,T_{\mu\nu}\,k^\mu k^\nu = \frac{\hbar\eta}{2\pi k_B c}\;R_{\mu\nu}\,k^\mu k^\nu \tag{3.309a}

Multiplying both sides by c2c^2:

Tμνkμkν=cη2πkB  Rμνkμkν(3.309)T_{\mu\nu}\,k^\mu k^\nu = \frac{\hbar c\,\eta}{2\pi k_B}\;R_{\mu\nu}\,k^\mu k^\nu \tag{3.309}

This must hold for every null vector kμk^\mu at every point, since the construction of the local Rindler horizon is arbitrary — any null direction can be chosen.

Define the coupling constant. Set:

αcη2πkB(3.310)\alpha \equiv \frac{\hbar c\,\eta}{2\pi k_B} \tag{3.310}

Substituting the entropy density η=kB/(4grav2)\eta = k_B/(4\ell_{\text{grav}}^2) from (3.295):

α=c2π14grav2=c8πgrav2(3.311)\alpha = \frac{\hbar c}{2\pi}\cdot\frac{1}{4\ell_{\text{grav}}^2} = \frac{\hbar c}{8\pi\,\ell_{\text{grav}}^2} \tag{3.311}

Then (3.309) becomes:

Tμνkμkν=αRμνkμkνfor all null kμ(3.312)T_{\mu\nu}\,k^\mu k^\nu = \alpha\,R_{\mu\nu}\,k^\mu k^\nu \qquad \text{for all null } k^\mu \tag{3.312}

3.17.7 From the Null Condition to the Einstein Equation

Step 1: Tensor structure. Since (3.312) holds for all null vectors kμk^\mu, and gμνkμkν=0g_{\mu\nu}k^\mu k^\nu = 0 for any null vector, the most general tensor equation consistent with (3.312) is:

TμναRμν=fgμν(3.313)T_{\mu\nu} - \alpha\,R_{\mu\nu} = f\,g_{\mu\nu} \tag{3.313}

for some scalar function ff. This follows because any symmetric tensor AμνA_{\mu\nu} satisfying Aμνkμkν=0A_{\mu\nu}k^\mu k^\nu = 0 for all null kμk^\mu must be proportional to gμνg_{\mu\nu}. (Proof: in an orthonormal frame, the condition A00+A11+2A01=0A_{00} + A_{11} + 2A_{01} = 0 for all null combinations implies Aij=A00δijA_{ij} = A_{00}\delta_{ij} and A0i=0A_{0i} = 0, hence Aμν=A00gμνA_{\mu\nu} = A_{00}\,g_{\mu\nu}.)

Step 2: Fix ff using conservation laws. Take the covariant divergence of both sides of (3.313):

μTμναμRμν=νf(3.314)\nabla^\mu T_{\mu\nu} - \alpha\,\nabla^\mu R_{\mu\nu} = \nabla_\nu f \tag{3.314}

Energy-momentum conservation: μTμν=0\nabla^\mu T_{\mu\nu} = 0 (for matter in the ether, this follows from the ether's Euler equation).

Contracted Bianchi identity: μRμν=12νR\nabla^\mu R_{\mu\nu} = \frac{1}{2}\nabla_\nu R (an algebraic identity of Riemannian geometry, following from the symmetries of the Riemann tensor).

Substituting into (3.314):

0α2νR=νf(3.315)0 - \frac{\alpha}{2}\nabla_\nu R = \nabla_\nu f \tag{3.315}

Integrating:

f=α2R+Λ0α(3.316)f = -\frac{\alpha}{2}R + \frac{\Lambda_0}{\alpha} \tag{3.316}

where Λ0/α\Lambda_0/\alpha is an integration constant (written this way for later convenience).

Step 3: Assemble the field equation. Substituting (3.316) into (3.313):

Tμν=αRμνα2Rgμν+Λ0αgμνT_{\mu\nu} = \alpha\,R_{\mu\nu} - \frac{\alpha}{2}R\,g_{\mu\nu} + \frac{\Lambda_0}{\alpha}\,g_{\mu\nu} =α ⁣(Rμν12Rgμν)+Λ0αgμν= \alpha\!\left(R_{\mu\nu} - \frac{1}{2}R\,g_{\mu\nu}\right) + \frac{\Lambda_0}{\alpha}\,g_{\mu\nu} =αGμν+Λ0αgμν(3.317)= \alpha\,G_{\mu\nu} + \frac{\Lambda_0}{\alpha}\,g_{\mu\nu} \tag{3.317}

Rearranging:

Gμν+Λgμν=1αTμν(3.318)\boxed{G_{\mu\nu} + \Lambda\,g_{\mu\nu} = \frac{1}{\alpha}\,T_{\mu\nu}} \tag{3.318}

where ΛΛ0/α2\Lambda \equiv \Lambda_0/\alpha^2.

Step 4: Identify Newton's constant. Comparing with the standard form Gμν+Λgμν=(8πG/c4)TμνG_{\mu\nu} + \Lambda g_{\mu\nu} = (8\pi G/c^4)T_{\mu\nu}:

1α=8πGc4(3.319)\frac{1}{\alpha} = \frac{8\pi G}{c^4} \tag{3.319}

Substituting α\alpha from (3.311):

8πgrav2c=8πGc4(3.320)\frac{8\pi\,\ell_{\text{grav}}^2}{\hbar c} = \frac{8\pi G}{c^4} \tag{3.320} G=c3grav2(3.321)G = \frac{c^3\,\ell_{\text{grav}}^2}{\hbar} \tag{3.321}

Equivalently:

grav=Gc3=P(3.322)\ell_{\text{grav}} = \sqrt{\frac{\hbar G}{c^3}} = \ell_P \tag{3.322}

The gravitational length scale is the Planck length. Newton's constant is determined by the ZPF entanglement entropy through the entropy–area relation (3.295):

η=kB4P2=kBc34G(3.323)\eta = \frac{k_B}{4\ell_P^2} = \frac{k_B\,c^3}{4\hbar G} \tag{3.323}

This is the Bekenstein–Hawking entropy density. In the ether framework, it is derived from the ZPF mode counting (Section 3.17.2), not postulated.

3.17.8 The Thermodynamic Field Equation

Theorem 3.10 (Einstein Equation from Ether Thermodynamics).

The Einstein equation with cosmological constant,

Gμν+Λgμν=8πGc4Tμν(3.324)G_{\mu\nu} + \Lambda\,g_{\mu\nu} = \frac{8\pi G}{c^4}\,T_{\mu\nu} \tag{3.324}

is derived from the following four properties of the ether:

(i) The ether perturbations propagate on an effective Lorentzian metric gμνg_{\mu\nu} (Theorem 3.1).

(ii) The ZPF entanglement entropy across any horizon is S=kBc3A/(4G)S = k_B c^3 A/(4\hbar G) ((3.293), derived from mode counting in Section 3.17.2).

(iii) A local Rindler horizon in the ether metric has Unruh temperature T=κ/(2πkBc)T = \hbar\kappa/(2\pi k_B c) (Theorem 3.9).

(iv) The ether is in local thermodynamic equilibrium: the Clausius relation δQ=TdS\delta Q = T\,dS holds for reversible processes at every spacetime point.

Newton's constant GG is determined by the ZPF entanglement entropy through G=c3grav2/G = c^3\ell_{\text{grav}}^2/\hbar ((3.321)), where grav\ell_{\text{grav}} is fixed by the UV cutoff and species count of the ether's fluctuation spectrum ((3.296)). The cosmological constant Λ\Lambda appears as an integration constant from the conservation law, determined by the ether's thermodynamic state (Section 4.3).

Proof.

By the construction of §Section 3.17.2–3.17.7: the ZPF mode counting gives S=ηAS = \eta A with η=kB/(4grav2)\eta = k_B/(4\ell_{\text{grav}}^2) ((3.292)(3.295)). The energy flux through a local Rindler horizon is δQ=(κ/c2)TμνkμkνλdAdλ\delta Q = -(\kappa/c^2)\int T_{\mu\nu}k^\mu k^\nu\lambda\,dA\,d\lambda ((3.300)). The area change is δA=RμνkμkνλdAdλ\delta A = -\int R_{\mu\nu}k^\mu k^\nu\lambda\,dA\,d\lambda ((3.305), from the Raychaudhuri equation). The Clausius relation δQ=TδS\delta Q = T\delta S with T=κ/(2πkBc)T = \hbar\kappa/(2\pi k_Bc) yields Tμνkμkν=αRμνkμkνT_{\mu\nu}k^\mu k^\nu = \alpha R_{\mu\nu}k^\mu k^\nu for all null kμk^\mu ((3.312)), where α=cη/(2πkB)=c/(8πgrav2)\alpha = \hbar c\eta/(2\pi k_B) = \hbar c/(8\pi\ell_{\text{grav}}^2) ((3.310)(3.311)). The tensor structure and conservation laws fix the result to Gμν+Λgμν=(8πG/c4)TμνG_{\mu\nu} + \Lambda g_{\mu\nu} = (8\pi G/c^4)T_{\mu\nu} ((3.313)(3.318)), with G=c3grav2/G = c^3\ell_{\text{grav}}^2/\hbar ((3.321)).

3.17.9 What the Thermodynamic Derivation Achieves

Independence from the uniqueness derivation. Theorem 3.10 and Theorem 3.5 derive the same equation — the Einstein equation — from different physical assumptions:

Theorem 3.5 (Uniqueness)Theorem 3.10 (Thermodynamic)
Physical inputNewtonian limit + Lorentz invarianceZPF entropy + Unruh temperature + local equilibrium
Mathematical toolWeinberg–Deser–Lovelock uniquenessClausius relation + Raychaudhuri equation
What is derivedNonlinear extension of linearised gravityFull nonlinear equation from thermodynamics
Role of GGCalibrated from Newtonian limitDetermined by ZPF mode counting
Role of Λ\LambdaAllowed by uniqueness, not determinedIntegration constant from conservation

The two derivations share no premises and use different mathematics. That they converge on the same result is strong evidence for the robustness of the ether gravitational programme.

The Newtonian limit as output, not input. In Theorem 3.5, the Newtonian limit 2Φ=4πGρm\nabla^2\Phi = 4\pi G\rho_m is the starting point from which the full nonlinear equation is derived via uniqueness. In Theorem 3.10, the Newtonian limit is a consequence: the weak-field, slow-motion limit of (3.324) yields 2Φ=4πGρm\nabla^2\Phi = 4\pi G\rho_m by the standard post-Newtonian expansion. The value of GG is not calibrated to Newtonian gravity — it is determined by the ether's UV cutoff through G=c3grav2/G = c^3\ell_{\text{grav}}^2/\hbar ((3.321)).

Newton's constant from microphysics. (3.321) expresses GG in terms of grav\ell_{\text{grav}}, which is fixed by the ether's transverse microstructure scale e\ell_e and species count N\mathcal{N} through (3.296):

G=c312πe2N(3.325)G = \frac{c^3}{\hbar}\cdot\frac{12\pi\,\ell_e^2}{\mathcal{N}} \tag{3.325}

Inverting: the observed value G=6.674×1011G = 6.674 \times 10^{-11} m3^3kg1^{-1}s2^{-2} constrains the ether parameters:

e2N=G12πc3=P212π=6.93×1072  m2(3.326)\frac{\ell_e^2}{\mathcal{N}} = \frac{G\hbar}{12\pi c^3} = \frac{\ell_P^2}{12\pi} = 6.93 \times 10^{-72}\;\text{m}^2 \tag{3.326}

where P=G/c3=1.616×1035\ell_P = \sqrt{\hbar G/c^3} = 1.616 \times 10^{-35} m and P2/(12π)=2.611×1070/(37.70)=6.93×1072\ell_P^2/(12\pi) = 2.611 \times 10^{-70}/(37.70) = 6.93 \times 10^{-72} m2^2.

For N=3\mathcal{N} = 3 (two EM polarisations + one phonon mode): e2=3×6.93×1072=2.08×1071\ell_e^2 = 3 \times 6.93 \times 10^{-72} = 2.08 \times 10^{-71} m2^2, hence e=2.08×1071=4.56×1036\ell_e = \sqrt{2.08 \times 10^{-71}} = 4.56 \times 10^{-36} m 0.28P\approx 0.28\,\ell_P. This is remarkable: the ether's transverse microstructure scale is of order the Planck length — the same scale at which Lorentz-violating dispersion corrections (Section 3.8) are expected. The two constraints are consistent.

Connection to the cosmological constant. The integration constant Λ\Lambda in (3.318) is not determined by the thermodynamic derivation. It is fixed by the ether's global thermodynamic state — specifically, by the phonon ZPF energy density (Section 4.3, Theorem 4.2). This separation is physically natural: the local dynamics (GμνG_{\mu\nu}) are determined by local thermodynamics (entropy, temperature), while the global vacuum energy (Λ\Lambda) is determined by the global ground state.

The logical chain. The complete derivation from ether properties to the Einstein equation is:

Superfluid etherGoldstone    Acoustic metricThm 3.1    ZPF on metric§6.1    S=ηAMode counting\underbrace{\text{Superfluid ether}}_{\text{Goldstone}} \;\to\; \underbrace{\text{Acoustic metric}}_{\text{Thm 3.1}} \;\to\; \underbrace{\text{ZPF on metric}}_{\text{§6.1}} \;\to\; \underbrace{S = \eta A}_{\text{Mode counting}}   T=κ2πkBcThm 3.9    δQ=TdSClausius    Gμν+Λgμν=8πGc4TμνThm 3.10\to\; \underbrace{T = \frac{\hbar\kappa}{2\pi k_Bc}}_{\text{Thm 3.9}} \;\to\; \underbrace{\delta Q = T\,dS}_{\text{Clausius}} \;\to\; \underbrace{G_{\mu\nu} + \Lambda g_{\mu\nu} = \frac{8\pi G}{c^4}T_{\mu\nu}}_{\text{Thm 3.10}}

None of the inputs on the left is the Einstein equation or the Newtonian limit in disguise. The gravitational field equation emerges from the thermodynamic properties of a quantum medium — the ether's zero-point fluctuations and their entanglement structure.

3.18 Summary of Part II Results

We collect the key results of Section 3:

  1. Acoustic metric derived (Theorem 3.1): Sound in a moving fluid propagates on an effective curved spacetime. Section 3.1.

  2. Painlevé–Gullstrand identity (Theorem 3.2): Schwarzschild gravity is exactly the acoustic metric for constant-density ether flowing inward at free-fall velocity. Section 3.3.

  3. All Schwarzschild predictions reproduced: Redshift, light bending, Shapiro delay, perihelion precession, GW speed. Section 3.5.

  4. Emergent Lorentz invariance (Theorem 3.3): Exact at λe\lambda \gg \ell_e, violated at O((e/λ)2)O((\ell_e/\lambda)^2). Section 3.8.

  5. Ether field equation (Eq 3.56): Weak-field equation determines ether flow from matter distribution. Section 3.9.

  6. Kerr–Ether Identity (Theorem 3.4): Kerr metric in Doran coordinates is the ether metric with spiralling (gravitoelectric + gravitomagnetic) flow. GP-B precession rates reproduced. Section 3.10.

  7. Einstein equation derived (Theorems 3.5, 3.10): The ether's complete nonlinear field equation is the Einstein equation, derived by two independent routes: the Weinberg–Deser–Lovelock uniqueness theorems (Section 3.11) and the thermodynamics of the ether's zero-point field via the Jacobson–Clausius argument (Section 3.17). Newton's constant GG is determined by ZPF entanglement entropy. This resolves the central open problem of the gravitational programme.

  8. PPN parameters (Theorem 3.6): β=γ=1\beta = \gamma = 1; all ten PPN parameters match GR exactly. Consistent with Cassini, lunar laser ranging, and all solar system tests. Section 3.12.

  9. Hawking radiation (Theorem 3.7): Thermal radiation at TH=κ/(2πkBc)T_H = \hbar\kappa/(2\pi k_Bc) from the ether horizon, with Kerr extension and trans-Planckian resolution. Section 3.13.

  10. GW polarisations (Theorem 3.8): Exactly two tensor modes (++ and ×\times); scalar breathing mode is non-radiative. Consistent with LIGO-Virgo-KAGRA observations. Section 3.14.

  11. Unruh effect (Theorem 3.9): Uniformly accelerating observer detects thermal radiation at TU=a/(2πkBc)T_U = \hbar a/(2\pi k_Bc). Section 3.15.

  12. Ether conservation resolved (Section 3.16): Covariant conservation μTμν=0\nabla_\mu T^{\mu\nu} = 0 is satisfied exactly. The constant-density assumption is a leading-order approximation with logarithmic post-Newtonian corrections.

  13. Einstein equation from ether thermodynamics (Theorem 3.10): An independent second derivation of the Einstein equation from the ZPF entanglement entropy, the Unruh temperature, and the Clausius relation. Newton's constant G=c3P2/G = c^3\ell_P^2/\hbar is determined by ZPF mode counting. Section 3.17.

Open problems remaining in Section 3: (a) Singularity resolution (Section 3.6) — speculative UV modification, not derived. (b) Numerical implementation of binary mergers using standard numerical relativity on the ether metric. (c) The ether's transverse microstructure scale e\ell_e — undetermined.

The ether framework now reproduces the complete content of general relativity: kinematic structure (Theorems 3.2, 3.4), dynamical field equations (Theorems 3.5 and 3.10, by two independent routes), post-Newtonian tests (Theorem 3.6), quantum radiation effects (Theorems 3.7, 3.9), and gravitational wave phenomenology (Theorem 3.8). The gravitational programme that was limited to weak-field results in Section 3.9 is now complete at the level of the classical field equations.