ANISOTROPIC SPACE DYNAMICS · CANONICAL THEORY

Shapiro Delay · Excess Optical Path and Propagation Counts

Establish a same-endpoint propagation reference from emission and reception, explain the first-order optical-path weight, endpoint integral, and round-trip conditions, and connect them to actual link measurements.

Based on the final manuscript · Chapter 2

TheoryTheory · DERIVEDReviewMathematical review · CONDITIONALEvidenceEvidence · CONSISTENTCanonicalYesStatus, review and sources

01The question posed by signal arrival counts

When a light or radio signal is sent to a distant location and its reception is recorded, the measured propagation quantity does not depend only on the straight-line distance drawn between the endpoints. If the link passes near a mass source such as the Sun, the effect of nonuniform space on the accumulated optical path must also be calculated. Shapiro delay asks how many additional propagation counts a signal accumulates relative to propagation without gravity between the same endpoints and in the same reference.

ASD interprets this increment as an excess reference optical path through a spatially stretched region. Matter changes the true spatial length of the path and the scale of the standard underlying the recording process. Converting the whole process to a common reference gives additional arrival counts. The local propagation speed of light remains cc. Light deflection measures the transverse gradient of the same optical path; this page calculates its accumulation along the path.

The measured quantity must first be specified. One-way propagation involves emission and reception endpoints and the connection between their references. A round-trip measurement records the total interval for the outgoing and returning signal. Both use the same background, but their events and paths cannot be interchanged without conditions. The calculation below first treats a fixed-endpoint vacuum link in a static background, then connects it to actual measurement.

02How the same spatial state enters propagation

Let the central source have mass MM and gravitational coupling coefficient G0G_0, and define ℓg=G0M/c2\ell_g=G_0M/c^2. The area radius rr is defined by the sphere area 4πr24\pi r^2. In the static spherically symmetric region outside the matter source with r>2ℓgr>2\ell_g, the manuscript adopts X=1−2ℓg/rX=1-2\ell_g/r, linear expansion coefficient Ω=X−1/2\Omega=X^{-1/2}, and dimensionless line-density coefficient Φ=Ω−1\Phi=\Omega^{-1}. Here Φ\Phi is not a quantum wave field, and ρ\rho will denote only a coordinate radius, not a volume density.

The true spatial line element in the orbital plane is dℓs2=X−1dr2+r2dφ2d\ell_s^2=X^{-1}dr^2+r^2d\varphi^2, where φ\varphi is the azimuthal angle. A far-field standard establishes counting parameter tt. The cycles accumulated by a local standard process satisfy dN=f0Φ dtdN=f_0\Phi\,dt, where f0f_0 is the far-field reference frequency. The locally calibrated speed is therefore v∗=Φ−1dℓs/dtv_*=\Phi^{-1}d\ell_s/dt. Setting v∗=cv_*=c for light gives the reference optical path dℓopt=Φ−1dℓsd\ell_{\rm opt}=\Phi^{-1}d\ell_s. True length and reference optical path have different roles and cannot be conflated with one Euclidean geometrical path.

For convenient integration, introduce an isotropic radial coordinate ρ\rho, related to the area radius by r=ρ(1+ℓg/2ρ)2r=\rho(1+\ell_g/2\rho)^2. In this representation, dℓopt=niso ds0d\ell_{\rm opt}=n_{\rm iso}\,ds_0, where ds0ds_0 is the reference Euclidean line element and nison_{\rm iso} weights each reference-length segment to give its optical path. This weight comes from the combined conversion of radial length and cycle reference. The coordinate change itself adds no physical effect.

A1 · Assumption

Constitutive relations and approximation used for propagation

Use the complete static optical path of Chapter 2, Eq. (2.26), and its weak-field form niso=1+2ℓg/ρ+O(ℓg2/ρ2)n_{\rm iso}=1+2\ell_g/\rho+O(\ell_g^2/\rho^2). The area radius rr and coordinate ρ\rho must not be interchanged in higher-order calculations.

This response of space and standard processes is a constitutive input to the model. Once it is specified, path integration gives the delay. Constancy of local cc alone does not fix the amount of excess optical path.

03Establishing the propagation reference without gravity

Let Γ\Gamma be the actual stationary light path connecting two fixed endpoints. Dividing each reference-optical-path segment by cc and summing gives

ASD-WEB-GRV-017
T[Γ]=1c∫Γniso ds0T[\Gamma]=\frac1c\int_\Gamma n_{\mathrm{iso}}\,ds_0

Mathematical result
Conditional on the stated inputs and domain. Manuscript numbering is separate from the website ID.
Chapter reference: Final collected manuscript · Chapter 2 §IV.6 (2.51) · ASD-BOOK-ddbade997b45

The functional T[Γ]T[\Gamma] is the propagation quantity for the entire path. To define an excess, the same pair of endpoints must be used in the same coordinates. Let their Euclidean straight line without gravity be Γ0\Gamma_0, with length R12R_{12}. The baseline propagation quantity is then R12/cR_{12}/c, and the one-way gravitational delay is defined by

ASD-WEB-GRV-018
ΔT=T−R12c\Delta T=T-\frac{R_{12}}c

Definition
Conditional on the stated inputs and domain. Manuscript numbering is separate from the website ID.
Chapter reference: Final collected manuscript · Chapter 2 §IV.6 (2.52) · ASD-BOOK-ddbade997b45

A2 · Assumption

A vacuum comparison with fixed endpoints

The background is static and the endpoints are fixed in the reference coordinates; rotation and propagation media are neglected. The no-gravity baseline uses R12/cR_{12}/c for the same endpoints, not a different endpoint pair or another definition of length.

This subtraction removes the propagation quantity associated with ordinary distance from the total, leaving the increment due to the gravitational background. It does not also remove every other link contribution from a measured total travel time. Endpoint motion, clock reference, and instrument response must still be treated in a specific measurement.

SCHEMATIC · FIRST-ORDER OPTICAL PATH

Distance and optical weighting

A ray passing a static spherical sourceEarth and target are at x = minus and plus four L. The straight reference path lies b above the source. Blue intensity indicates the relative first-order optical correction, not a measured ray deflection.bSource · MEarthTarget−4L+4L
Conceptual illustration; not experimental data. Both models use the same endpoints at each slider setting. The first-order delay weights the straight reference path; it is not calculated by drawing a longer bent ray.
R₁₂ / L
8
Δℓopt / (2ℓg)
4.1894
ΔT / (2G₀M/c³)
4.1894

Here x₁ = x₂ = 4L and the ASD correction is 2 asinh(4L/b). Changing b also changes the schematic endpoint positions. Values are dimensionless first-order model calculations, valid when ℓg/b ≪ 1. The complete reference optical length differs from radial true spatial length.

The two modes in the illustration retain the same endpoints, with color showing the relative along-path weight of niso−1n_{\rm iso}-1. This is a conceptual illustration and first-order model calculation, not experimental data or a fit to an actual spacecraft link. It uses an arbitrary reference length LL rather than assumed Earth–Sun or spacecraft distances. Retaining the straight path Γ0\Gamma_0 corresponds to the first-order method below; the appearance of the illustration does not give a physical higher-order bending magnitude.

04Why the first-order integral can use a straight line

The actual light path bends, so why can the delay still be calculated along Γ0\Gamma_0? The essential distinction is between changing the path and changing its optical-path weight, expanding both to the same order. Write n=1+δnn=1+\delta n and Γ=Γ0+δΓ\Gamma=\Gamma_0+\delta\Gamma, where δn\delta n and the path perturbation are both first order in the weak field.

A straight line between fixed endpoints already makes Euclidean length stationary, so δ∫ds0=0\delta\int ds_0=0. The purely geometrical length increment from a small deflection begins at higher order. Multiplying the first-order weight δn\delta n by the first-order path change also exceeds the present accuracy. Thus the first-order delay needs only

ΔT=1c∫Γ0(niso−1) ds0+higher-order terms.\Delta T=\frac1c\int_{\Gamma_0}(n_{\rm iso}-1)\,ds_0+\text{higher-order terms}.

This is the construction of manuscript Eq. (2.53). The true spatial path and the reference conversion of the standard process have already entered nison_{\rm iso}; integration along a reference straight line does not discard them. The excess optical path is read primarily through the along-path weight. Equating it entirely with the extra Euclidean distance caused by a bent ray would omit the first-order term here.

05From the endpoint integral to a logarithmic relation

In the reference coordinate plane, place the central source at the origin and take the unperturbed path at y=b>0y=b>0, parametrized by xx. The quantity bb is the minimum reference distance from this straight line to the center: the impact parameter of the present weak-field calculation. Place emission and reception on opposite sides of closest approach, at x=−x1x=-x_1 and x=x2x=x_2, with x1,x2>0x_1,x_2>0. Their coordinate radii are ρi=xi2+b2\rho_i=\sqrt{x_i^2+b^2}, while along the path ρ=x2+b2\rho=\sqrt{x^2+b^2}.

Substituting niso−1≃2ℓg/ρn_{\rm iso}-1\simeq2\ell_g/\rho into the preceding expression and using ds0=dxds_0=dx gives

ASD-WEB-GRV-019
ΔT≃2G0Mc3∫−x1x2dxx2+b2\Delta T\simeq\frac{2G_0M}{c^3}\int_{-x_1}^{x_2}\frac{dx}{\sqrt{x^2+b^2}}

Mathematical result
Conditional on the stated inputs and domain. Manuscript numbering is separate from the website ID.
Chapter reference: Final collected manuscript · Chapter 2 §IV.6 (2.53)—(2.54); first-order weak-field integral · ASD-BOOK-ddbade997b45

An antiderivative is

∫dxx2+b2=ln⁡x+x2+b2b.\int\frac{dx}{\sqrt{x^2+b^2}} =\ln\frac{x+\sqrt{x^2+b^2}}b.

Normalizing lengths in the logarithm by bb makes its argument dimensionless. Substituting both endpoints and denoting the integral by II gives

I=ln⁡x2+ρ2ρ1−x1.I=\ln\frac{x_2+\rho_2}{\rho_1-x_1}.

Since (ρ1−x1)(ρ1+x1)=b2(\rho_1-x_1)(\rho_1+x_1)=b^2, the contribution from the negative endpoint can be rewritten using a product of positive lengths:

ASD-WEB-GRV-020
ΔT=2G0Mc3ln⁡ ⁣[(ρ1+x1)(ρ2+x2)b2]\Delta T=\frac{2G_0M}{c^3}\ln\!\left[\frac{(\rho_1+x_1)(\rho_2+x_2)}{b^2}\right]

Mathematical result
Equality is at first-order accuracy, with endpoints across closest approach.
Chapter reference: Final collected manuscript · Chapter 2 §IV.6 (2.55) · ASD-BOOK-ddbade997b45

For the same reference straight line, R12=x1+x2R_{12}=x_1+x_2. These endpoint relations let the same result be written using only the two endpoint radii and their separation:

ASD-WEB-GRV-021
ΔT=2G0Mc3ln⁡ ⁣(ρ1+ρ2+R12ρ1+ρ2−R12)\Delta T=\frac{2G_0M}{c^3}\ln\!\left(\frac{\rho_1+\rho_2+R_{12}}{\rho_1+\rho_2-R_{12}}\right)

Mathematical result
Equality is at first-order accuracy; all endpoint distances use one coordinate convention.
Chapter reference: Final collected manuscript · Chapter 2 §IV.6 (2.56)—(2.57) · ASD-BOOK-ddbade997b45

Final equation (2.57) explicitly supplies the exact algebraic identity behind this rewriting:

(ρ1+x1)(ρ2+x2)b2=ρ1+ρ2+R12ρ1+ρ2−R12.\frac{(\rho_1+x_1)(\rho_2+x_2)}{b^2} =\frac{\rho_1+\rho_2+R_{12}}{\rho_1+\rho_2-R_{12}}.

This identity is exact for the stated endpoint geometry. The gravitational delay that multiplies its logarithm remains a first-order weak-field calculation.

The latter expression is an algebraic rearrangement of the former, with no additional propagation effect. Equalities in both are understood at the first-order weak-field accuracy of this section. They retain the integration endpoints but are not exact closed forms for complete strong-field propagation. The quantities ρ1\rho_1, ρ2\rho_2, and R12R_{12} must all be given in the same reference coordinates.

06Distant endpoints and a round-trip link

When both endpoints lie far from the closest-approach region, ρ1,ρ2≫b\rho_1,\rho_2\gg b and xi≃ρix_i\simeq\rho_i. The endpoint expression reduces to

ASD-WEB-GRV-022
ΔT≃2G0Mc3ln⁡ ⁣(4ρ1ρ2b2)\Delta T\simeq\frac{2G_0M}{c^3}\ln\!\left(\frac{4\rho_1\rho_2}{b^2}\right)

Mathematical result
Distant-endpoint asymptote of the first-order weak-field result, ρ₁,ρ₂≫b. Final (2.57) is the exact identity between endpoint logarithm arguments.
Chapter reference: Final collected manuscript · Chapter 2 §IV.6 (2.58) and the following distant-endpoint asymptote; not final equation (2.57) · ASD-BOOK-ddbade997b45

This approximation highlights two physical ingredients: source mass sets the scale of the excess optical path, while the closest-approach distance and endpoint positions determine its accumulation. The quantity G0M/c3G_0M/c^3 has dimensions of time, the logarithm has a dimensionless argument, and the increment vanishes for M→0M\to0.

A3 · Assumption

Conditions for doubling a one-way result

The static vacuum one-way result can be multiplied directly by two only if endpoint positions and geometry remain approximately unchanged between outgoing and returning propagation. Actual moving endpoints, clock references, and medium terms require separate modeling.

Under this condition, the round-trip delay is

ASD-WEB-GRV-023
ΔTround=2ΔT=4G0Mc3ln⁡ ⁣(ρ1+ρ2+R12ρ1+ρ2−R12)\Delta T_{\mathrm{round}}=2\Delta T=\frac{4G_0M}{c^3}\ln\!\left(\frac{\rho_1+\rho_2+R_{12}}{\rho_1+\rho_2-R_{12}}\right)

Mathematical result
Full endpoint formula at first weak-field order for fixed endpoints and equal outgoing/returning geometry; no additional distant-endpoint assumption.
Chapter reference: Final collected manuscript · Chapter 2 §IV.6 (2.58) · ASD-BOOK-ddbade997b45

The registered expression now retains the full endpoint ratio in final (2.58); it does not impose ρi≫b\rho_i\gg b. Only after that additional limit does it reduce to 4G0Mln⁡(4ρ1ρ2/b2)/c34G_0M\ln(4\rho_1\rho_2/b^2)/c^3.

If the ground station or spacecraft has moved appreciably by the time the signal is retransmitted at the spacecraft, outgoing and returning propagation must each use their corresponding events and paths before being combined in a common counting reference. The static doubling relation explains the connection between one-way and round-trip quantities; it does not replace a raw ranging model for a moving spacecraft.

07Connecting to actual experimental comparisons

A Shapiro measurement connects propagation theory to emission, retransmission, and reception events. In addition to the gravitational term, the measurement equation must include endpoint orbits, station clocks and frequency references, propagation media, and instrument effects. Radio links near the Sun particularly require treatment of plasma and related effects. In the Cassini radio experiment, for example, link frequency variations are related to corresponding changes in round-trip light time; the quantity compared is the signal after instrument and propagation treatment. See the NASA/JPL experiment report.

This page derives a static first-order delay from the ASD spatial optical path. With endpoints, coordinates, and approximation order matched, it has the same mathematical form as the comparison-theory result. The result itself therefore does not discriminate between ASD and general relativity. No independent refit of Cassini data has been performed here, and the interactive illustration is not treated as an apparatus model. Observational references and the scope of calculation are recorded in gravity test entry GRV-EXP-003.

08Scope and connections to further calculations

The integrals above apply to a static spherically symmetric vacuum exterior, with the entire path in the weak field and the small-deflection expansion valid. The explicit endpoint integral uses endpoints on opposite sides of closest approach; distant-endpoint and round-trip relations add their own approximation conditions. Higher precision requires a consistent expansion of the complete optical path and endpoint conditions, including source multipoles, rotation, path bending, and actual link terms. Replacing a coordinate radius by the area radius in just one formula does not provide that expansion.

ASD connects two propagation phenomena through the same spatial state: transverse optical-path variation changes ray direction, while accumulation along the path changes arrival counts. The common background is described in the gravity overview, the optical-path coordinate conversion in light deflection, and the scale and counting relations of standard processes in gravitational redshift. Strong-field propagation requires the complete exterior optical model and its scope as described under static compact objects.

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§IV.6 (2.51)—(2.58)

Retain the full continuous explanation; adopt the corresponding constitutive inputs, results and domain of final Chapter 2.

Conditions retained in this adoption

  • Fixed G₀; isolated, static, spherically symmetric, uncharged exterior.
  • Areal radius, actual spatial length and reference optical path are defined separately.
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  • Microscopic source matching, dynamical strong fields and full boundary-state dynamics remain open.

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ASD: Shapiro Delay · Excess Optical Path and Propagation Counts. ASD-GRV-SHAPIRO-DELAY-EN. Version 1.0.0; 2026-10-24. https://asd-physics.org/en/theory/gravity/shapiro-delay. §IV.6 (2.51)—(2.58). Source ASD-BOOK-ddbade997b45.

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