Holographic Noise with Causal Structure

quantitative

Prediction

The discrete relational invariant network underlying continuum spacetime introduces irreducible position uncertainty at the Planck scale. This uncertainty manifests as holographic noise — random fluctuations in length measurements that cannot be eliminated by any improvement in measurement technology.

The unique, testable signature: the noise has a specific anisotropic cross-correlation structure. Two interferometers at relative angle β\beta show cross-correlated noise with overlap reduction function Γ(β)=cosβ\Gamma(\beta) = \cos\beta. This angular dependence — not the absolute amplitude — is the framework’s distinctive prediction and the key experimental target.

Quantitative Summary

QuantityFormulaValue
Position uncertainty (length LL)Δx=αHPL\Delta x = \sqrt{\alpha_H \ell_P L}for L=4L = 4 km at αH=1/4\alpha_H = 1/4
Michelson strain PSDSh(Mich)=4αHP/cS_h^{(\text{Mich})} = 4\alpha_H \ell_P / c5.4×1044\lesssim 5.4 \times 10^{-44} Hz1^{-1} at Holometer bound
Amplitude coefficientαH\alpha_H0.24\lesssim 0.24 (Holometer, tight); natural target 1/4\sim 1/4
Michelson cross-correlationΓ(β)=cosβ\Gamma(\beta) = \cos\betaTestable angular pattern
Single-arm cross-correlationγ(α)=cosα\gamma(\alpha) = \cos\alphaBetween arms at angle α\alpha, sharing a beamsplitter
Frequency spectrumWhite (flat) for f<c/(2L)f < c/(2L)No frequency dependence

Derivation from Axioms

Step 1: The Relational Invariant Network as a Causal Set

From the derivation chain: AxiomsTime as Phase OrderingSpeed of LightGravityHolographic Entropy Bound.

The microscopic structure of spacetime is a labelled causal set (C,,λ)(C, \prec, \lambda):

The causal set approximates a Lorentzian manifold (M,gμν)(M, g_{\mu\nu}) at scales P\gg \ell_P. The fundamental density of elements is one per Planck 4-volume:

ρ=1P4=c3G4.1×10139 m4\rho = \frac{1}{\ell_P^4} = \frac{c^3}{\hbar G} \approx 4.1 \times 10^{139} \text{ m}^{-4}

This follows from the Holographic Entropy Bound: the maximum information density in any region is one bit per Planck cell.

Step 2: Position Uncertainty from Discrete Structure

A spacetime point PP in the continuum description corresponds to a cluster of causal set elements. A length measurement between two points P1P_1 and P2P_2 along a null geodesic of spatial separation LL involves counting causal set elements along the geodesic.

Proposition (Holographic scaling). The number of independent causal set elements along a null geodesic of spatial length LL is:

Nnull=LPN_{\text{null}} = \frac{L}{\ell_P}

Each element contributes an independent random displacement δxi\delta x_i with δxi=0\langle \delta x_i \rangle = 0 and δxi2=αHP2\langle \delta x_i^2 \rangle = \alpha_H \ell_P^2, where αH\alpha_H is a dimensionless O(1) coefficient encoding the causal set statistics.

By the random walk:

(Δx)2null=NαHP2=αHPL\langle (\Delta x)^2 \rangle_{\text{null}} = N \cdot \alpha_H \ell_P^2 = \alpha_H \ell_P L

This is the holographic scaling: position uncertainty grows as PL\sqrt{\ell_P L}, not as P\ell_P. The PL\sqrt{\ell_P L} scaling is a rigorous consequence of CLT applied to Poisson cells (Causal Set Statistics, Proposition 2.2); the amplitude αH\alpha_H depends on the specific length estimator and is not yet derived from first principles (see Causal Set Statistics, Heuristic 2.3).

Step 3: The Shared-Origin Displacement and the Relational Invariant at the Beamsplitter

The key structural feature that makes holographic noise anisotropic at macroscopic arm lengths — and distinguishes this prediction from Hogan’s isotropic model — is that the two arms of a Michelson share a relational invariant established at the beamsplitter. This is nonlocal by construction and is the mechanism behind the cross-correlation between arms.

Proposition 3.1 (Beamsplitter as Type III interaction). When a coherent laser pulse is split by a 50/50 beamsplitter into two outgoing modes along arm directions n^a\hat{n}_a and n^b\hat{n}_b, the splitting is a Type III interaction (Three Interaction Types) that generates a relational invariant IabI_{ab} between the two arm states.

Proof sketch. A symmetric beamsplitter maps a single-mode coherent state onto the entangled two-mode state (a+b)/2(|a\rangle + |b\rangle)/\sqrt{2} — this is the textbook quantum-optics result. By Entanglement Proposition 1.3, any such entangled pair corresponds to a relational invariant IabI_{ab} in the framework’s coherence geometry, with coherence content C(Iab)\mathcal{C}(I_{ab}) equal to the entanglement entropy of the reduced state (Theorem 2.1 of the same derivation). The coherence channel γabch\gamma_{ab}^{\text{ch}} carrying IabI_{ab} (ER=EPR Definition 1.1) is anchored at the beamsplitter vertex. \square

Proposition 3.2 (Shared-origin displacement structure). The length fluctuations in the two arms are projections of a single random vector displacement δX\delta\mathbf{X} at the beamsplitter vertex, shared by both arms through the relational invariant IabI_{ab}:

δLa=n^aδX,δLb=n^bδX\delta L_a = -\hat{n}_a \cdot \delta\mathbf{X}, \qquad \delta L_b = -\hat{n}_b \cdot \delta\mathbf{X}

The sign convention reflects that moving the beamsplitter vertex toward a mirror by n^aδX\hat{n}_a \cdot \delta\mathbf{X} shortens arm aa by the same amount. By rotational and translational invariance of the observer network (Lorentz Invariance), the covariance of δX\delta\mathbf{X} is isotropic:

δXiδXj=13δX2δij\langle \delta X_i \, \delta X_j \rangle = \frac{1}{3}\,\langle |\delta\mathbf{X}|^2\rangle \, \delta_{ij}

The structure is shared, not local. The cross-correlation between arms cannot arise from independent local sampling along disjoint paths: two arms from a common origin share only the origin cell at scales LPL \gg \ell_P, which would give zero cross-correlation. The cross-correlation exists because the two arms are linked by the relational invariant IabI_{ab} generated at the beamsplitter — a genuinely nonlocal coherence-topological connection, the same structural object that underlies entanglement and its ER=EPR dual. The shared structure does not require spatial overlap of the arms’ spacetime neighborhoods; it requires only that both arms originate from a common Type III interaction at the beamsplitter.

Setting the amplitude. The holographic position uncertainty at distance LL from a reference point is αHPL\sqrt{\alpha_H \ell_P L} (from Causal Set Statistics Proposition 2.2, rigorous PL\sqrt{\ell_P L} scaling). Identifying the beamsplitter as the reference vertex and the mirror as the measurement endpoint:

13δX2=2αHPL\frac{1}{3}\,\langle |\delta\mathbf{X}|^2\rangle = 2\alpha_H\,\ell_P\,L

(the factor of 2 comes from the round-trip path; see Step 4). This matches the single-arm variance and ensures consistency across Steps 2, 4, and 5.

Consistency with Heuristic 2.3. The isotropic projection δL2=13δX2\delta L^2 = \tfrac{1}{3}\langle|\delta\mathbf{X}|^2\rangle (per-component variance, by isotropy) matches the scalar-accumulation calculation in Causal Set Statistics Heuristic 2.3 exactly when the bridge rule “one boundary bit ↔ P2\ell_P^2 of length variance” is read as per-component variance of the minimal observer’s 3D position. This reading is forced by the Compton-wavelength interpretation of the minimal observer: λC(mP)=P\lambda_C(m_P) = \ell_P is the minimum localization scale per direction, so a 3D minimum-uncertainty wavepacket at this scale has δxi2P2\langle\delta x_i^2\rangle \sim \ell_P^2 for each component separately and δx23P2\langle|\delta\mathbf{x}|^2\rangle \sim 3\ell_P^2 for the total magnitude. Summing over Neff=L/(4P)N_{\text{eff}} = L/(4\ell_P) independent minimal observers gives per-component variance NeffP2=LP/4N_{\text{eff}}\ell_P^2 = L\ell_P/4 and total magnitude 3NeffP2=3LP/43N_{\text{eff}}\ell_P^2 = 3L\ell_P/4, returning αH=1/4\alpha_H = 1/4 from both pictures (1-way; double for round-trip). The two derivations are consistent bases for the same isotropic fluctuation, not competing predictions — see the Remark under Heuristic 2.3 for details.

Step 4: Single-Arm Noise Power

For a single interferometer arm of length LL along direction n^\hat{n}, light travels out and back. The total path is 2L2L. The single-arm variance is:

(δL)2=2αHPL\langle (\delta L)^2 \rangle = 2\alpha_H \ell_P L

This follows equivalently from the projection of the shared-origin displacement δX\delta\mathbf{X} in Step 3 (with the normalization fixed there), or from a direct integration over Planck cells along the round-trip path via CLT on Poisson sprinklings (Causal Set Statistics, Proposition 2.2). The two descriptions are consistent because the relational invariant connecting the beamsplitter to the mirror is the same coherence-channel object that the causal-set elements along the round-trip null path carry (ER=EPR Definition 1.1). The random variable can be attributed to the beamsplitter vertex or distributed along the arm path — both attributions describe the same relational invariant and give the same single-arm variance.

The strain is h=δL/Lh = \delta L / L, with variance:

h2=2αHPL\langle h^2 \rangle = \frac{2\alpha_H \ell_P}{L}

The strain power spectral density (one-sided, for frequencies f<c/(2L)f < c/(2L)):

Sh(arm)(f)=2αHPc\boxed{S_h^{(\text{arm})}(f) = \frac{2\alpha_H \ell_P}{c}}

Key point: This is the same for all arm orientations. Single-arm noise power is isotropic because each arm probes the causal set along its own null direction.

Step 5: Cross-Correlation Between Arms — The Angular Signature

The anisotropy appears in the cross-correlation between two arms. Let arms aa and bb share a common beamsplitter vertex and be oriented along n^a\hat{n}_a and n^b\hat{n}_b at angle α\alpha.

Theorem 5.1 (Single-arm cross-correlation). The noise cross-spectrum between two arms at relative angle α\alpha is:

Cab(f)=2αHPccosα\boxed{C_{ab}(f) = \frac{2\alpha_H \ell_P}{c} \cdot \cos\alpha}

or equivalently, the overlap reduction function at the single-arm level is:

γ(α)=δLaδLbδLa2=cosα\gamma(\alpha) = \frac{\langle \delta L_a \, \delta L_b \rangle}{\langle \delta L_a^2 \rangle} = \cos\alpha

Proof. From Step 3 (Proposition 3.2), the two arms share a single isotropic random displacement δX\delta\mathbf{X} at the beamsplitter vertex, with δLa=n^aδX\delta L_a = -\hat{n}_a \cdot \delta\mathbf{X} and δLb=n^bδX\delta L_b = -\hat{n}_b \cdot \delta\mathbf{X}. Direct computation:

δLaδLb=n^ain^bjδXiδXj=13δX2(n^an^b)=13δX2cosα\langle \delta L_a\,\delta L_b\rangle = \hat{n}_a^i \hat{n}_b^j \langle \delta X_i\,\delta X_j\rangle = \frac{1}{3}\langle|\delta\mathbf{X}|^2\rangle\,(\hat{n}_a \cdot \hat{n}_b) = \frac{1}{3}\langle|\delta\mathbf{X}|^2\rangle\,\cos\alpha

using isotropy δXiδXj=13δX2δij\langle \delta X_i \delta X_j\rangle = \tfrac{1}{3}\langle|\delta\mathbf{X}|^2\rangle\,\delta_{ij} from Proposition 3.2. Similarly, δLa2=13δX2\langle \delta L_a^2\rangle = \tfrac{1}{3}\langle|\delta\mathbf{X}|^2\rangle, so the ratio is cosα\cos\alpha. With the normalization 13δX2=2αHPL\tfrac{1}{3}\langle|\delta\mathbf{X}|^2\rangle = 2\alpha_H\ell_P L from Step 3, the cross-spectrum follows. \square

Angular values.

Remark (why rotational invariance forces this shape). For any rank-1 vector noise field with rotationally-invariant 2-point function, the cross-correlation between two arms from a common origin is a+bcosαa + b\cos\alpha for some constants a,ba, b. The pure cosα\cos\alpha form corresponds to the minimal assumption — no rotationally-invariant scalar “breathing mode” component. A scalar component would shift aa without affecting the cos β harmonic in Step 7, so the distinctive angular signature Γ(β)=cosβ\Gamma(\beta) = \cos\beta is robust to this choice. Under the simplest (vector-only) model, a=0a = 0 and the formula is exact.

Step 6: Michelson Interferometer — Differential Measurement

A Michelson interferometer with perpendicular arms along x^\hat{x} and y^\hat{y} measures the differential strain:

hMich=δLxδLyLh_{\text{Mich}} = \frac{\delta L_x - \delta L_y}{L}

The noise power, using Cxy=(2αHP/c)cos(π/2)=0C_{xy} = (2\alpha_H\ell_P/c)\cos(\pi/2) = 0 from Theorem 5.1:

Sh(Mich)=Sxx+Syy2Cxy=2αHPc+2αHPc0=4αHPcS_h^{(\text{Mich})} = S_{xx} + S_{yy} - 2C_{xy} = \frac{2\alpha_H \ell_P}{c} + \frac{2\alpha_H \ell_P}{c} - 0 = \frac{4\alpha_H \ell_P}{c}

Result: A single Michelson sees holographic noise at Sh(Mich)=4αHP/cS_h^{(\text{Mich})} = 4\alpha_H \ell_P/c, independent of its orientation in space. The two perpendicular arms contribute independently because γ(π/2)=0\gamma(\pi/2) = 0 — orthogonal projections of an isotropic random vector are uncorrelated.

Step 7: The Overlap Reduction Function — Two Interferometers

Theorem (Michelson-to-Michelson cross-correlation). Two co-located Michelson interferometers at relative angle β\beta have cross-correlated noise:

Γ(β)=cosβ\boxed{\Gamma(\beta) = \cos\beta}

Derivation. Let interferometer 1 have arms along (x^,y^)(\hat{x}, \hat{y}) and interferometer 2 have arms along (x^,y^)(\hat{x}', \hat{y}') where x^=cosβx^+sinβy^\hat{x}' = \cos\beta\,\hat{x} + \sin\beta\,\hat{y}.

h1h2L2=δLxδLxδLxδLyδLyδLx+δLyδLy\langle h_1 h_2 \rangle L^2 = \langle \delta L_x \delta L_{x'}\rangle - \langle \delta L_x \delta L_{y'}\rangle - \langle \delta L_y \delta L_{x'}\rangle + \langle \delta L_y \delta L_{y'}\rangle

Using Cab=(2αHP/c)cos(αab)C_{ab} = (2\alpha_H\ell_P/c)\cos(\alpha_{ab}) from Theorem 5.1 with angles:

h1h2L2=2αHPc[cosβ(sinβ)sinβ+cosβ]=2αHPc2cosβ=4αHPccosβ\langle h_1 h_2 \rangle L^2 = \frac{2\alpha_H\ell_P}{c}\Big[\cos\beta - (-\sin\beta) - \sin\beta + \cos\beta\Big] = \frac{2\alpha_H\ell_P}{c}\cdot 2\cos\beta = \frac{4\alpha_H\ell_P}{c}\cos\beta

Normalizing by Sh(Mich)=4αHP/cS_h^{(\text{Mich})} = 4\alpha_H\ell_P/c:

Γ(β)=h1h2Sh(Mich)=cosβ\Gamma(\beta) = \frac{\langle h_1 h_2 \rangle}{S_h^{(\text{Mich})}} = \cos\beta \quad \square

Relative angle β\betaΓ(β)\Gamma(\beta)Configuration
0°1.001.00Parallel (Holometer)
30°30°0.870.87
45°45°0.710.71
60°60°0.500.50LISA arm pairs
90°90°0.000.00Perpendicular
180°180°1.00-1.00Anti-parallel arm 1

Symmetries and Sanity Checks

Arm convention. Throughout Steps 3–7 an “arm” is a directed line from the beamsplitter vertex to a mirror, parameterized by a unit direction vector n^\hat{n}. The length fluctuation projects the shared-origin displacement onto the arm direction: δLn^=n^δX\delta L_{\hat{n}} = -\hat{n} \cdot \delta\mathbf{X}. Reversing the arm direction reverses the sign of the projection: δLn^=δLn^\delta L_{-\hat{n}} = -\delta L_{\hat{n}}. Physically, “arm along n^-\hat{n}” means the mirror sits at Ln^-L\hat{n} rather than +Ln^+L\hat{n}, which is a different physical configuration (the mirror is on the opposite side of the beamsplitter), not a relabeling of the same arm.

Behavior under physical rotations of Mich 2. Let Mich 2’s “arm 1” make angle β\beta with Mich 1’s “arm 1” (so its arm 2 is at β+π/2\beta + \pi/2). Three rotation cases:

The full period of Γ(β)\Gamma(\beta) is 2π2\pi. There is no shorter period — in particular, Γ\Gamma does NOT return to itself under ββ+π/2\beta \to \beta + \pi/2.

Independent check at β=π/2\beta = \pi/2. A direct calculation that does not invoke the γ(α)=cosα\gamma(\alpha) = \cos\alpha formula: at β=π/2\beta = \pi/2, Mich 2’s arms are y^\hat y and x^-\hat x. Then h2=δLy^δLx^=δLy^+δLx^h_2 = \delta L_{\hat y} - \delta L_{-\hat x} = \delta L_{\hat y} + \delta L_{\hat x} and h1h2L2=(δLx^δLy^)(δLx^+δLy^)=δLx^2δLy^2=0\langle h_1 h_2\rangle L^2 = \langle (\delta L_{\hat x} - \delta L_{\hat y})(\delta L_{\hat x} + \delta L_{\hat y})\rangle = \langle \delta L_{\hat x}^2\rangle - \langle \delta L_{\hat y}^2\rangle = 0 by isotropy of the shared-origin displacement (δXiδXjδij\langle \delta X_i \delta X_j\rangle \propto \delta_{ij}, so δLn^2\langle \delta L_{\hat n}^2\rangle is the same for any unit n^\hat n). The cross-terms δLx^δLy^\delta L_{\hat x}\delta L_{\hat y} and δLy^δLx^\delta L_{\hat y}\delta L_{\hat x} are equal and cancel exactly. The vanishing of Γ(π/2)\Gamma(\pi/2) therefore follows from isotropy alone, providing a sanity check independent of the cosine formula.

Comparison with a stochastic gravitational-wave background. The angular pattern Γ(β)=cosβ\Gamma(\beta) = \cos\beta is the response of an interferometer to a vector noise field — a rank-1 (dipolar) object. A standard isotropic stochastic gravitational-wave background, by contrast, is a rank-2 (spin-2 / quadrupolar) tensor field, and its overlap reduction function for two co-located Michelsons has period π/2\pi/2 in the relative angle (returning to its starting value when one detector is rotated by π/2\pi/2, because GW strain transforms in the spin-2 representation of SO(2)SO(2)). Holographic noise distinguishes itself from a GW background by its period: dipolar (period 2π2\pi, with a sign flip at π\pi) rather than quadrupolar (period π/2\pi/2). This is a clean qualitative discriminator independent of the absolute amplitude — even a low-statistics measurement of the angular pattern can rule out one or the other.

Step 8: Separated Detectors

The derivation of γ(α)=cosα\gamma(\alpha) = \cos\alpha in Step 5 relies on the two arms of a Michelson sharing a single random displacement δX\delta\mathbf{X} at a common beamsplitter vertex. For two interferometers whose beamsplitter vertices are separated by spatial distance dd, the relevant question is: how do the random displacements at two distinct vertices δX1\delta\mathbf{X}_1 and δX2\delta\mathbf{X}_2 correlate?

Theorem 8.1 (Separated-vertex zero cross-correlation). For two beamsplitter vertices at macroscopic spatial separation dPd \gg \ell_P, the random displacements generated by the Type III interactions at each vertex are uncorrelated at leading order:

δXi(1)(t1)δXj(2)(t2)=O ⁣(P3d3)(isotropic tensor)\boxed{\langle \delta X_i^{(1)}(t_1)\,\delta X_j^{(2)}(t_2) \rangle = O\!\left(\frac{\ell_P^3}{d^3}\right) \cdot \text{(isotropic tensor)}}

independent of frequency. Consequently the overlap reduction function between separated Michelson interferometers is zero to leading order, regardless of their relative orientation:

Γsep(β,d)0(dP).\Gamma_{\text{sep}}(\beta, d) \approx 0 \qquad (d \gg \ell_P).

Proof. By Relational Invariants Theorem 2.1, a Type III interaction generates a relational invariant II anchored at the spacetime event of that interaction. By Theorem 4.1 of the same derivation, II is irreducible — it cannot be decomposed as a sum f(σ1)+g(σ2)f(\sigma_1) + g(\sigma_2) of independent contributions from separate upstream sources. By Entanglement Proposition 1.3, the relational invariant corresponds to an entangled coherence structure anchored at that event.

The shared-origin displacement of Step 3 works because both output arms of a single beamsplitter inherit from one relational invariant generated at one Type III interaction. The covariance δXiδXj\langle \delta X_i\,\delta X_j \rangle for the same-vertex case follows from the irreducibility of that single invariant plus rotational invariance of the coherence measure.

Two distinct beamsplitter events at distinct vertices are two distinct Type III interactions and therefore generate two distinct, independent relational invariants I(1)I^{(1)} and I(2)I^{(2)}. The irreducibility property applies to each invariant separately; there is no framework-level mechanism that links them into a single joint invariant at leading order.

Possible subleading channels, each strictly subdominant at macroscopic dd:

(i) Poisson cell overlap. The reconstruction of each vertex’s position from the local causal set samples a volume of Planck cells near the vertex. By the independence of Planck cells in a Poisson sprinkling (Causal Set Statistics), cells near vertex 1 and cells near vertex 2 at separation dPd \gg \ell_P are independent. The contribution to the cross-covariance from the (measure-zero in the limit, O(P3/d3)O(\ell_P^3/d^3) at finite dd) overlap region of near-vertex cells is negligible for any macroscopic dd.

(ii) Shared ambient observers in the broader hierarchy. Both beamsplitters sit within a higher-level observer (e.g., Earth or the local cosmic web at bootstrap level >NBS> N_{\text{BS}}), which contributes to both vertices’ local coherence environments. This is a shared upstream relational invariant, but it manifests as a global metric perturbation at the two vertices — the same class of effect as a passing gravitational wave, not as shared holographic noise. The framework’s definition of holographic noise (rank-1 vector fluctuation from Planck-scale causal set structure, Step 2) explicitly excludes such large-scale metric correlations, which belong to the GW sector.

(iii) Optical coherence of the laser line. A common laser source feeding both beamsplitters establishes classical phase correlation in the input coherent states, not a shared geometric relational invariant. The beamsplitter-generated invariants I(1)I^{(1)} and I(2)I^{(2)} are created at each beamsplitter event from the local substrate, not inherited from the laser source in a way that mixes their geometric displacements.

Each channel contributes at most O(P3/d3)O(\ell_P^3/d^3) relative to the single-vertex variance O(αHPL)O(\alpha_H \ell_P L). For any macroscopic dd of experimental interest, the leading-order cross-correlation is zero. \square

Corollary 8.2 (Separated vs. co-located: a qualitative discriminator). The holographic-noise signature is qualitatively different between co-located and separated detector configurations:

ConfigurationHolographic noiseSpin-2 GW background
Co-located, relative angle β\betaΓ(β)=cosβ\Gamma(\beta) = \cos\beta (period 2π2\pi)ΓGW(β)\Gamma_{\text{GW}}(\beta) quadrupolar (period π/2\pi/2)
Separated by dPd \gg \ell_PΓsep=0\Gamma_{\text{sep}} = 0 (to leading order)ΓGW(d,β)0\Gamma_{\text{GW}}(d, \beta) \neq 0 (standard overlap reduction function)

The separated-detector behavior is a sharper discriminator than the angular pattern alone: a GW background exhibits a specific non-zero overlap reduction function between separated detectors (e.g., Flanagan’s curve for LIGO H–L), while holographic noise predicts approximately zero. This is because GWs are propagating fields that reach both detectors coherently, whereas holographic noise is a local property of each vertex’s relational invariant.

Causality argument (weaker, still instructive). Independent of Theorem 8.1, causality alone provides a necessary condition: two beamsplitter vertices at spatial separation dd are causally disconnected over time intervals shorter than d/cd/c, so frequency components above fcohc/(2πd)f_{\text{coh}} \sim c/(2\pi d) cannot maintain phase coherence between the two vertices for any underlying noise model. Theorem 8.1 shows that the framework’s structure is stricter: cross-correlation is zero at all frequencies, not just above fcohf_{\text{coh}}.

Implication for LIGO Hanford–Livingston (d3000d \approx 3000 km, β90°\beta \approx 90°): no holographic-noise cross-correlation at leading order — sharper than the causality-only conclusion. The LIGO H–L pair is not a useful probe of this prediction.

Implication for LISA (arm length L=d2.5×109L = d \approx 2.5 \times 10^9 m, TDI channels anchored at different spacecraft vertices): no cross-correlation between TDI channels at leading order — sharper than the causality-only conclusion, which at LISA’s observation band (1\sim 1 mHz fcoh0.02\ll f_{\text{coh}} \approx 0.02 Hz) would have predicted approximately full cos60°\cos 60° transmission. The framework-specific prediction is null.

Confrontation with the Holometer

The Holometer Experiment

The Holometer Chou et al., 2017 operated two co-located, co-aligned (β=0°\beta = 0°) 40-meter Michelson interferometers, searching for correlated length fluctuations at 1–13 MHz.

Published constraint: SL<8.4×1041S_L < 8.4 \times 10^{-41} m²/Hz at 95% CL.

Comparison with the Prediction

The predicted displacement power spectrum for β=0\beta = 0:

SL=L2Γ(0)Sh(Mich)=L24αHPcS_L = L^2 \cdot \Gamma(0) \cdot S_h^{(\text{Mich})} = L^2 \cdot \frac{4\alpha_H\ell_P}{c}

With L=40L = 40 m:

SL=(40)2×4αH×1.616×10353×108=3.45×1040αH m2/HzS_L = (40)^2 \times \frac{4\alpha_H \times 1.616 \times 10^{-35}}{3 \times 10^8} = 3.45 \times 10^{-40}\,\alpha_H \text{ m}^2\text{/Hz}

The Holometer constraint gives:

αH<8.4×10413.45×10400.24\alpha_H < \frac{8.4 \times 10^{-41}}{3.45 \times 10^{-40}} \approx 0.24

Result: The Holometer constrains αH0.24\alpha_H \lesssim 0.24. The framework’s natural target from the holographic bound heuristic is αH1/4=0.25\alpha_H \sim 1/4 = 0.25 (see Causal Set Statistics Heuristic 2.3). The prediction therefore sits essentially at the Holometer bound — the natural target value is marginally disfavored (at 3%\sim 3\% tension) and any value αH0.24\alpha_H \lesssim 0.24 is consistent. The framework is in a knife-edge regime: a Holometer-class experiment with a factor-2 improvement in sensitivity would directly confirm or rule out the natural target.

Why αH=1/4\alpha_H = 1/4 Is a Framework-Specific Prediction

The holographic bound gives αH=1/4\alpha_H = 1/4 via the following route: the Planck-tube causal diamond containing a length-LL geodesic has boundary area Amax=LPA_{\max} = L \cdot \ell_P, which by Bekenstein–Hawking encodes at most Neff=Amax/(4P2)=L/(4P)N_{\text{eff}} = A_{\max}/(4\ell_P^2) = L/(4\ell_P) independent bits — a factor of 44 below the naive bulk count. Treating these NeffN_{\text{eff}} bits as the independent fluctuation degrees of freedom contributing P2\ell_P^2 each to the length variance gives δL2=PL/4\delta L^2 = \ell_P L/4, hence αH=1/4\alpha_H = 1/4.

This is a framework-specific prediction, not a generic holographic expectation. Its specificity comes from treating the holographic count as a fluctuation-DOF count rather than a bare information-capacity cap: under the framework’s relational-invariant coarse-graining, boundary bits are coarse-grained relational invariants whose fluctuations are what the interferometer measures. Under the standard causet-literature position (Poisson substrate elements each contributing independent fluctuations, no holographic coarse-graining), the naive answer is αH1\alpha_H \sim 1 — a factor of 4 larger.

InterpretationFluctuation sourcePredicted αH\alpha_H
Framework (relational-invariant coarse-graining)Holographically-counted bits, Neff=A/(4P2)N_{\text{eff}} = A/(4\ell_P^2)1/41/4
Generic causet (Poisson substrate)Substrate Planck cells, Nbulk=A/P2N_{\text{bulk}} = A/\ell_P^21\sim 1

The Holometer experiment constrains αH0.24\alpha_H \lesssim 0.24, consistent with the framework’s 1/41/4 (within 3% tension) and inconsistent with the generic-causet 1\sim 1. The existing null already discriminates in favor of the framework interpretation — the knife-edge regime at 1/41/4 is the expected position of a specific framework prediction, not a generic heuristic.

Third view — the 1/41/4 as a QEC code rate. The table above places the 1/41/4 factor between the holographically-counted boundary bits (Neff=A/(4P2)N_{\text{eff}} = A/(4\ell_P^2)) and the naive Planck-cell substrate count (Nbulk=A/P2N_{\text{bulk}} = A/\ell_P^2) — a ratio that is identified by Observer as an Error-Correcting Code Corollary 4.1.1 as the code rate of the observer’s spatial-axis HaPPY-family factor of the observer-projection CPTP map. Under that reading the 1/41/4 appearing in Heuristic 2.3 (this prediction), in the holographic entropy bound, and in the Bekenstein–Hawking entropy are three views of a single QEC invariant: the substrate-to-code redundancy of the spatial-axis factor (see Remark 4.1.2 of that derivation).

One open item remains around the precise 1/41/4 value. The apparent scalar-vs-vector bridge-rule ambiguity — whether ”P2\ell_P^2 per bit” attaches to the scalar variance δL2\delta L^2 or to the 3D vector magnitude δX2|\delta\mathbf{X}|^2 — is resolved by the Compton-wavelength interpretation of the minimal observer: λC(mP)=P\lambda_C(m_P) = \ell_P is the minimum localization scale per direction, so each bit contributes P2\ell_P^2 to the per-component variance (equivalently, to the along-direction scalar variance by isotropy). Under this reading both Heuristic 2.3 and Proposition 3.2’s isotropic projection δL2=(1/3)δX2\delta L^2 = (1/3)|\delta\mathbf{X}|^2 return αH=1/4\alpha_H = 1/4 (see the Consistency remark under Step 3 above, and the Remark under Causal Set Statistics Heuristic 2.3). The remaining open item is the one tracked in Causal Set Statistics Open Gap 1: a direct causet-literature estimator (Brightwell–Gregory longest-chain, Myrheim–Meyer interval-count, or tube-count) does not naturally yield 1/41/4; the framework’s specific value requires the Heuristic 2.3 composite construction (holographic count + bridge rule), not a generic Poisson-estimator calculation.

Current status. At αH=1/4\alpha_H = 1/4 the Michelson PSD is:

Sh(Mich)=Pc5.4×1044 Hz1S_h^{(\text{Mich})} = \frac{\ell_P}{c} \approx 5.4 \times 10^{-44} \text{ Hz}^{-1}

which sits at the Holometer bound (marginally 3% above the published 95% CL, within the framework’s O(1) theoretical uncertainty on the overall Heuristic 2.3 substitution). The framework is in a knife-edge regime: a Holometer-class experiment with factor-2 improved sensitivity at β=0\beta = 0 would directly test the 1/41/4 value. Test 1 below (rotatable cross-correlation) provides an independent probe of the distinctive Γ(β)=cosβ\Gamma(\beta) = \cos\beta angular pattern, free of the absolute amplitude uncertainty.

Experimental Tests

Test 1: Rotatable Cross-Correlation (The Definitive Test)

Configuration: Two co-located Michelson interferometers, one rotatable relative to the other.

Protocol:

  1. Measure cross-correlated noise S12(β)S_{12}(\beta) at relative angles β=0°,30°,45°,60°,90°\beta = 0°, 30°, 45°, 60°, 90°
  2. Fit the angular dependence to S12(β)=S0cosβS_{12}(\beta) = S_0 \cdot \cos\beta

Predictions:

S12(0°)S12(45°)=1cos45°=21.41\frac{S_{12}(0°)}{S_{12}(45°)} = \frac{1}{\cos 45°} = \sqrt{2} \approx 1.41

S12(90°)=0(null test)S_{12}(90°) = 0 \quad \text{(null test)}

Key advantage: The angular RATIO is independent of αH\alpha_H. This matters especially because αH\alpha_H itself is currently an O(1) parameter, not a rigorously derived constant (see “Why αH1/4\alpha_H \sim 1/4” above). The cosβ\cos\beta shape is the true experimental target — it tests the structural prediction of the framework without depending on the undetermined amplitude coefficient. Isotropic noise (e.g., Hogan’s model) gives Γ=1\Gamma = 1 for all β\beta; the framework predicts Γ=cosβ\Gamma = \cos\beta. A measured ratio S12(0°)/S12(45°)=2S_{12}(0°)/S_{12}(45°) = \sqrt{2} and null at 90°90° would support the prediction regardless of what absolute amplitude emerges.

Required sensitivity: To detect Sh(Mich)=P/cS_h^{(\text{Mich})} = \ell_P/c (at αH=1/4\alpha_H = 1/4) in cross-correlation with SNR = 5 over T=1T = 1 year at bandwidth Δf=1\Delta f = 1 MHz:

SNR=ΓSh(Mich)S1S22TΔf\text{SNR} = \frac{|\Gamma| \cdot S_h^{(\text{Mich})}}{\sqrt{S_1 S_2}} \cdot \sqrt{2T\Delta f}

With S1=S2=SnS_1 = S_2 = S_n (instrumental noise):

Sn<ΓSh(Mich)2TΔf5=1×5.4×1044×2×3.15×107×1065S_n < \frac{|\Gamma| \cdot S_h^{(\text{Mich})} \cdot \sqrt{2T\Delta f}}{5} = \frac{1 \times 5.4\times10^{-44} \times \sqrt{2 \times 3.15\times10^7 \times 10^6}}{5}

=5.4×1044×7.9×1065=8.6×1038 Hz1= \frac{5.4\times10^{-44} \times 7.9\times10^6}{5} = 8.6 \times 10^{-38} \text{ Hz}^{-1}

Sn<2.9×1019 /Hz\sqrt{S_n} < 2.9 \times 10^{-19} \text{ /}\sqrt{\text{Hz}}

This is achievable with current technology (the Holometer achieved 1018\sim 10^{-18} m/√Hz displacement sensitivity with 40m arms).

Test 2: LISA Angular Channels

Configuration: LISA’s three arms at 60°60° form three Michelson-equivalent channels via Time Delay Interferometry (TDI).

Predicted cross-channel structure: Each TDI channel is anchored at a different spacecraft beamsplitter vertex at spatial separation d=2.5×109d = 2.5 \times 10^9 m. By Theorem 8.1, separated beamsplitter vertices generate independent relational invariants at leading order, so the cross-correlation between TDI channels is null for holographic noise:

Γ12=Γ23=Γ130(leading order)\Gamma_{12} = \Gamma_{23} = \Gamma_{13} \approx 0 \qquad (\text{leading order})

This is stronger than the causality-only bound, which at LISA’s 1 mHz band (fcoh0.02\ll f_{\text{coh}} \approx 0.02 Hz) would have allowed approximately full cos60°=0.5\cos 60° = 0.5 transmission. The framework’s Type-III-interaction structure forces zero regardless of frequency.

Consequence for holographic-noise detection with LISA: LISA is not a useful probe of holographic noise via cross-channel correlation. The three TDI channels should have independent holographic-noise contributions at the single-channel (auto-correlation) level Sh(Mich)=4αHP/cS_h^{(\text{Mich})} = 4\alpha_H\ell_P/c, but cross-channel stacking provides no SNR improvement. LISA’s auto-correlation sensitivity at 1 mHz (Sn1020/Hz\sqrt{S_n} \sim 10^{-20}/\sqrt{\text{Hz}}) is many orders of magnitude above the predicted Sh(Mich)7×1022/Hz\sqrt{S_h^{(\text{Mich})}} \sim 7 \times 10^{-22}/\sqrt{\text{Hz}} amplitude, so LISA cannot detect holographic noise even in auto-correlation.

Diagnostic use: if an excess correlated signal is detected in LISA’s TDI cross-correlations, it cannot be holographic noise — the framework predicts zero. This turns LISA into a potential falsifier of interpretations that would attribute LISA cross-correlations to holographic origin, but not a probe of the signal itself.

The existing gravitational-wave detector network can search for an isotropic stochastic background. Holographic noise contributes a correlated signal between co-located detectors but, by Theorem 8.1, zero correlation between separated detectors at leading order — stronger than the causality-only cutoff and independent of the causality coherence frequency fcohc/(2πd)f_{\text{coh}} \sim c/(2\pi d).

Predicted cross-correlations across the network: For all current LIGO–Virgo–KAGRA pairs (separations 1000\sim 10001000010000 km), holographic noise gives Γ0\Gamma \approx 0 at leading order. Any correlated stochastic signal detected in cross-correlation between separated detectors therefore cannot be holographic noise under the framework.

The qualitative diagnostic: If an excess stochastic signal is found in the network, the framework’s separated-vertex null makes this a clean distinguishing test:

Observed signalConsistent with
Non-zero cross-correlation between separated detectors (e.g., H–L, H–V, L–V)GW background, instrumental correlation, astrophysical foreground — not holographic noise
Zero cross-correlation plus elevated auto-correlation at the Sh(Mich)=4αHP/cS_h^{(\text{Mich})} = 4\alpha_H\ell_P/c levelConsistent with holographic noise (though auto-correlation alone is hard to distinguish from instrumental noise)

The holographic-noise rank-1 vector field is, per Theorem 8.1, a local-vertex fluctuation — it does not propagate between detectors the way a spin-2 GW field does. This is a sharper test than the angular-period discriminator of Step 7: the separated-detector null is model-independent given the framework’s Type III structure.

Test 4: Next-Generation Dedicated Experiment

Optimal configuration for the framework’s prediction:

ParameterValueRationale
Arm lengthL=40L = 40 mMatches Holometer; maximizes SNR at MHz
Number of interferometers3One fixed, two at different angles
Angles0°, 45°45°, 90°90°Probes Γ=1\Gamma = 1, 0.710.71, 00
Frequency band1–10 MHzWhite noise, above seismic
Strain sensitivity<1019< 10^{-19}/√HzFactor 10 beyond Holometer
Integration time1 yearSNR ∝ √T

Expected outcome: The 90°90° channel provides a null measurement (control); the 0° and 45°45° channels should show a ratio of 2\sqrt{2} in cross-correlation amplitude if the prediction is correct.

Comparison with Competing Predictions

FeatureObserver-centrismHogan holographic noiseLQG spacetime foamString theory
Noise amplitudeαHPL\sqrt{\alpha_H \ell_P L}PL\sqrt{\ell_P L}(P/L)n\sim (\ell_P/L)^n, n>1n > 1No prediction
Angular dependenceΓ(β)=cosβ\Gamma(\beta) = \cos\betaIsotropic (Γ=1\Gamma = 1)IsotropicN/A
Frequency spectrumWhite (f<c/2Lf < c/2L)WhiteModel-dependentN/A
Co-located nullΓ(90°)=0\Gamma(90°) = 0No null angleNo null angleN/A
Separated-vertex correlationZero (dPd \gg \ell_P; Theorem 8.1)Isotropic — no separation dependenceModel-dependentN/A
Holometer statusαH0.24\alpha_H \lesssim 0.24 (knife-edge)ExcludedAmplitude too smallNot falsifiable
Decisive testRotate baselineAlready testedNeeds 103×10^3\times sensitivityNone

Critical distinction: Hogan’s holographic noise model predicts isotropic cross-correlation (Γ=1\Gamma = 1) and was ruled out by the Holometer. The observer-centrism prediction has the same amplitude scaling but ANISOTROPIC cross-correlation (Γ(β)=cosβ\Gamma(\beta) = \cos\beta), making it consistent with the Holometer null result at αH0.24\alpha_H \lesssim 0.24 and testable by a rotatable configuration. The natural target αH1/4\alpha_H \sim 1/4 sits essentially at the Holometer bound, making the framework highly predictive: a factor-2 sensitivity improvement at β=0\beta = 0 would be decisive.

Numerical Reference

Fundamental constants:

ConstantValue
P=G/c3\ell_P = \sqrt{\hbar G/c^3}1.616×10351.616 \times 10^{-35} m
tP=P/ct_P = \ell_P/c5.391×10445.391 \times 10^{-44} s
P/c\ell_P/c5.391×10445.391 \times 10^{-44} Hz1^{-1}

Predicted noise levels (at αH=1/4\alpha_H = 1/4, using Sh(Mich)=4αHP/c=P/cS_h^{(\text{Mich})} = 4\alpha_H\ell_P/c = \ell_P/c):

QuantityFormulaValue
Michelson strain PSDSh(Mich)=P/cS_h^{(\text{Mich})} = \ell_P/c5.4×10445.4 \times 10^{-44} Hz1^{-1}
Strain amplitudeSh(Mich)\sqrt{S_h^{(\text{Mich})}}7.3×10227.3 \times 10^{-22} /√Hz
Displacement PSD (L=40L = 40 m)L2Sh(Mich)L^2 S_h^{(\text{Mich})}8.6×10418.6 \times 10^{-41} m²/Hz
Displacement PSD (L=4L = 4 km)L2Sh(Mich)L^2 S_h^{(\text{Mich})}8.6×10358.6 \times 10^{-35} m²/Hz
Position uncertainty (L=4L = 4 km)αHPL\sqrt{\alpha_H \ell_P L}1.27×10161.27 \times 10^{-16} m
Position uncertainty (L=2.5×106L = 2.5 \times 10^6 km)αHPL\sqrt{\alpha_H \ell_P L}1.0×10131.0 \times 10^{-13} m

Derivation Chain Status

The derivation chain threads through axioms (derived), multiple rigorous intermediate results, and three structural postulates. Status per step:

  1. Coherence Conservation (Axiom 1) — derived
  2. Observer Definition (Axiom 2) — derived
  3. Loop Closure (Axiom 3) — derived
  4. Minimal Observer → discrete structure — derived
  5. Relational Invariants → network — derived
  6. Time → causal ordering — derived
  7. Speed of Light → null structure — provisional (depends on speed-of-light-s1)
  8. Gravity → Planck scale — provisional
  9. Holographic Entropy Bound → area scaling — provisional (depends on area-scaling-s1)
  10. Causal Set Statistics → amplitude coefficient αH\alpha_Hprovisional (inherits from 7, 9; αH\alpha_H itself is an O(1) coefficient with natural target 1/4\sim 1/4 from a heuristic holographic substitution — not rigorously derived)
  11. Entanglement + ER=EPR → nonlocal shared-origin structure at the beamsplitter — derived (these derivations are already at rigorous status)
  12. Rotational invariance of the shared-origin displacement → γ(α)=cosα\gamma(\alpha) = \cos\alpha → angular pattern Γ(β)=cosβ\Gamma(\beta) = \cos\betaderived (Theorem 5.1): the single-arm cross-correlation is rigorously obtained from the isotropic covariance of the displacement at the beamsplitter vertex, which is itself grounded in the relational invariant generated by the Type III interaction at the beamsplitter (Proposition 3.1)
  13. Irreducibility of distinct relational invariants (Relational Invariants Theorem 4.1) → Γsep(β,d)0\Gamma_{\text{sep}}(\beta, d) \approx 0 for separated vertices (Theorem 8.1) — derived: separated Type III interactions generate independent relational invariants, forcing zero cross-correlation at leading order O(P3/d3)O(\ell_P^3/d^3) for dPd \gg \ell_P. Stronger than the causality-only cutoff.

This prediction inherits the provisional status of its upstream dependencies at steps 7–10. One open item remains load-bearing:

Rigor Assessment

Rigorously established:

Heuristic / natural-target (not derived):

Modeling assumptions (reasonable but not uniquely forced):

Separated-vertex cross-correlation (previously open, now derived at Theorem 8.1): cross-correlation between displacements at two distinct beamsplitter vertices at macroscopic separation dPd \gg \ell_P is zero at leading order (O(P3/d3)O(\ell_P^3/d^3)), independent of frequency. This is stronger than the causality-only cutoff and gives Tests 2 (LISA) and 3 (LIGO network) a null prediction rather than a quantitative non-zero cross-correlation. The result is forced by the irreducibility of relational invariants at distinct Type III interactions (Relational Invariants Theorem 4.1).

Open:

Open Gaps

  1. Exact amplitude from causal set statistics: The first-principles αH\alpha_H question is structural rather than computational. The framework’s PL\sqrt{\ell_P L} scaling and αH1/4\alpha_H \sim 1/4 both presuppose a count-based estimator (Planck-thickness tube of cells along the path), where the sum-of-independents variance gives αH=1\alpha_H = 1 trivially and the holographic substitution rule of Causal Set Statistics Heuristic 2.3 reduces it to 1/41/4. Resolving αH\alpha_H requires either deriving the holographic substitution rule from the framework’s axioms or constructing a non-Poisson causet model with explicit holographic correlations. The natural Brightwell–Gregory longest-chain Monte Carlo on Poisson-sprinkled 4D Minkowski is not a route to αH\alpha_H — the longest-chain length is an extreme-value statistic with sub-linear variance, not a sum-of-independents. See Causal Set Statistics Open Gap 1 for the current framing.
  2. Formalize the beamsplitter-as-Type III-interaction lemma: Proposition 3.1 asserts that a 50/50 beamsplitter generates a relational invariant with the specific shared-displacement structure used in Step 5. This is grounded in standard quantum optics plus the Entanglement and ER=EPR derivations, but a short explicit lemma tying the three together (coherent input → beamsplitter unitary → entangled output → relational invariant with isotropic vector structure) would sharpen the foundation of the γ(α) = cos α result.
  3. Scalar vs. vector composition of the shared displacement: The current derivation uses a pure rank-1 vector model (Proposition 3.2), giving γ(α)=cosα\gamma(\alpha) = \cos\alpha exactly. A rotationally-invariant scalar component would produce γ(α)=a+bcosα\gamma(\alpha) = a + b\cos\alpha with a>0a > 0. Both give the same Γ(β)=cosβ\Gamma(\beta) = \cos\beta at the Michelson level, but distinguishing them requires a more detailed substrate model.
  4. Higher-order correlations: The prediction focuses on two-point correlations. Higher-point statistics (three-point, four-point) of the holographic noise would provide additional model-independent tests.
  5. Cosmological corrections: In an expanding universe with Hubble parameter HH, the causal structure is modified. The noise PSD may acquire a correction (HP/c)\sim (H\ell_P/c) at cosmological baselines.
  6. Curved spacetime generalization: Near massive bodies, the noise should be modified by the local curvature. The prediction in Schwarzschild spacetime would be relevant for tests using GPS or pulsar timing.
  7. Connection to gravitational wave memory: Holographic noise at very low frequencies (f0f \to 0) might contribute to a stochastic gravitational wave background with specific polarization properties distinguishable from astrophysical sources.