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21 CHC-CCL

Task-Fixed pi Readout within a Declared Solar-System Calibration Window

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A declared-class calibration-layer hypothesis is formulated on a Solar-System window and is used to test whether a present horizon-scale quantity admits a task-fixed Earth-unit path-normalization readout under one shared curvature-layering map for a path-normalization calibration variable and the local clock-rate factor. The exact symbolic core carried by the path-harmonic Earth-unit path-normalization chain is isolated here as the paper-internal core, while the wider witness-backed calibration layer remains conditional on the same declared witness data. The archived manuscript remains authoritative for exact notation, equations, assumptions, and exclusions.

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01

Introduction and scope

A present-day comoving horizon scale is commonly quoted as a radius of order 464646--474747 billion light-years, while the Earth-inferred cosmic age is commonly taken as τ013.8 Gyr\tau_0\simeq 13.8~\mathrm{Gyr}\tau_0\simeq 13.8~\mathrm{Gyr}. These quantities are operationally distinct: τ0\tau_0\tau_0 is tied to local clocks and calibration conventions, whereas a present-day horizon radius D0D_0D_0 depends on a chosen horizon definition and a chosen parameter set. Reference cosmological parameter sets are quoted in primary cosmological analyses [citation].

Scope..

No FLRW dynamics or standard horizon integrals are re-derived. The problem addressed here is narrower: whether a declared Solar-System calibration-layer hypothesis with shared curvature layering in propagation and clock rate can yield a declared-class relation between a present horizon-scale quantity D0D_0D_0 and the Earth-inferred age τ0\tau_0\tau_0 once the admissible window, witness package, and completion task are fixed. The exact symbolic chain is the paper-internal core, whereas any wider DSN-to-Earth-unit calibration claim remains conditional on a witness-backed set of delay, angular, and clock data that is stated but not certified here. The shared map below is used only as a local calibration-layer hypothesis on that declared Solar-System window, and no general propagation law, general clock law, or cosmological horizon theorem is claimed outside that declared class.

Target quantity..

The quantity D0D_0D_0 is treated as a present-day horizon radius expressed in Earth light-year units (Gly). It is not a directly measured local observable; it is a derived scale whose meaning depends on stated conventions. The question is whether the adopted calibration class yields a declared-class relation between D0D_0D_0 and τ0\tau_0\tau_0 after the Solar-System window, the admissibility conditions, and the completion task have been fixed.

Conditional statement..

If (i) a scale-free Solar-System layering profile with exponent q=3/4q=3/4q=3/4 is admissible, (ii) the effective refractive geometry n(r)1/κ(r)n(r)\propto 1/\kappa(r)n(r)\propto 1/\kappa(r) satisfies the solar-window Herglotz monotonicity condition introduced below, and (iii) the same boundary-normalized κ(r)\kappa(r)\kappa(r) survives the witness package consisting of delay reconstruction, angular witness consistency, and clock-channel equality/loop-exactness testing, then the declared calibration class yields

D0=τ0π2F(3/4).D_0=\tau_0\,\pi^2\,F(3/4).
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D_0=\tau_0\,\pi^2\,F(3/4).

Here FFF is the closed-form Solar-System path factor derived in Sec. reference. A numerical value is assigned only after fixing τ0\tau_0\tau_0, rr_\odotr_\odot, rr_\oplusr_\oplus, the adopted unit conventions, and the comparison horizon convention; that later evaluation is not part of the declared-class theorem chain. The numerical proximity of the resulting evaluation to commonly quoted present-horizon scales is used only as an internal consistency check within the adopted class. If any witness object required by the declared package is absent, unavailable on the same boundary-normalized window, or fails the stated admissibility rule, then no Earth-unit calibration is assigned on that window.

Logical separation of the calibration steps..

The final calibration is conjunctive. Delay/range reconstruction, exponent fixing, witness acceptance, task-fixed completion, normalization-class selection, and horizon readout are distinct steps, and none is silently absorbed into another. In particular, the exponent q=3/4q=3/4q=3/4 is fixed only within the shell-content/extensivity premises of Sec. reference, not by DSN data alone; the completion constant C=π\mathcal C=\pi\mathcal C=\pi is fixed only by the declared task in Sec. reference; and the equality Vread/c=πV_{\rm read}/c_\oplus=\piV_{\rm read}/c_\oplus=\pi is read only after the declared normalization class has been selected by the witness package.

Companion metrology-reference note..

The CCL/PTM-VP0 metrology-reference result supports only CCL-METROLOGY-REFERENCE-CHECK-SATISFIED on the declared BIPM--NIST/CODATA--IAU reference-check surface, with the shared umbrella label CCL-PTM-VP0-REFERENCE-CHECK-SATISFIED. It confirms the declared symbolic/metrological chain for the reference constants used by the CCL/PTM readout; it does not certify any wider delay--angular--clock empirical witness outside the declared certificate surface, does not assign the Earth-unit calibration outside the declared class, and does not convert the construction into a general propagation, clock, horizon, or SI-redefinition theorem.

Logical dependency of the final readout..

The Earth-unit calibration consequence uses the following dependency order: Lemma reference fixes the path-harmonic reading of additive travel time; Proposition reference fixes q=3/4q=3/4q=3/4 only under the stated scale-free shell-extensivity premise; Theorem reference fixes the task-bound completion constant; Corollary reference supplies the class-bound path-normalization readout Vread/c=πV_{\rm read}/c_\oplus=\piV_{\rm read}/c_\oplus=\pi; Proposition reference gives R=π2F(3/4)R=\pi^2F(3/4)R=\pi^2F(3/4); and Corollary reference gives D0=τ0π2F(3/4)D_0=\tau_0\pi^2F(3/4)D_0=\tau_0\pi^2F(3/4). None of these implications is read outside its declared hypotheses.

Figure or table content is omitted from the web reader; use the canonical manuscript for the exact object.

Figure or table content is omitted from the web reader; use the canonical manuscript for the exact object.

Symbolic dependency boundary..

Table reference records the symbolic implication structure of the declared calibration layer. Delay/range, angular/VLBI, and clock-transfer channels test admissibility of the declared Solar-System map, while the listed lemma, proposition, theorem, and corollaries carry the class-bound calibration consequence under the stated hypotheses.

Figure or table content is omitted from the web reader; use the canonical manuscript for the exact object.

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02

Operational map: shared curvature layering in path-normalization and clock

Shared distortion factorEarth-unit path-normalization readout as a path-harmonic meanEarth-unit ratio

Shared distortion factor Let TTT denote global time and τ\tau\tau denote local (Earth) clock time. We introduce a bounded Solar-System curvature-layering proxy Ξ(r)[0,1)\Xiloc(r)\in[0,1)\Xiloc(r)\in[0,1) on the declared propagation window (Definition reference).

definition: Bounded Solar-System curvature-layering proxy. The symbol Ξ(r)\Xiloc(r)\Xiloc(r) denotes an operational curvature-layering measure used only through the shared distortion map developed here. It is bounded by construction on the declared Solar-System window, and it is not identified here with the unbounded CHC phase-gradient measure Ξ\Xi\Xi used in dynamical CHC papers. Any analysis that would require values outside [0,1)[0,1)[0,1) lies outside the admissible scope of the present calibration map and is not interpreted within the framework developed here.

Define

κ(r)1Ξ(r)(0,1].\kappa(r)\equiv \sqrt{1-\Xiloc(r)}\in(0,1].
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\kappa(r)\equiv \sqrt{1-\Xiloc(r)}\in(0,1].

definition: Declared shared calibration-map hypothesis. A path-normalization calibration variable and a local clock-rate factor share the same curvature-layering factor:

v(r)=Vκ(r),dτ(r)=κ(r)dT,v(r)=V\,\kappa(r),\qquad d\tau(r)=\kappa(r)\,dT,
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v(r)=V\,\kappa(r),\qquad d\tau(r)=\kappa(r)\,dT,

where v(r)v(r)v(r) and VVV are internal calibration-layer variables used only inside the declared travel-time functional. They are not modified metric light speeds, local group velocities, signal velocities, or universal propagation speeds.

remark: Single-geometry admissibility of the shared map. Equation reference is used here only as a local calibration-layer hypothesis on the declared Solar-System window. It is not promoted in this paper to a general CHC propagation law, a general clock law, or a cosmological distance law. Within that declared window, propagation observables and clock observables are read through one common geometric structure with no second-clock effect. In the Ehlers--Pirani--Schild viewpoint, light propagation fixes a conformal structure, free fall fixes a projective structure, and the absence of a second-clock effect is what permits a common Lorentzian metric representative [citation]. This motivates treating reference as a hypothesis to be tested by cross-channel equality rather than as an unconditional identification.

Earth-unit path-normalization readout as a path-harmonic mean Solar-System path-normalization readouts are induced by additive travel time along a declared path. We fix the Solar-System propagation window by adopting external conventions for its boundary constants.

definition: Declared Solar-System window and fixed boundary constants. We take raur_\oplus\equiv \mathrm{au}r_\oplus\equiv \mathrm{au} to denote the heliocentric radius scale of Earth's orbit, where au\mathrm{au}\mathrm{au} is defined exactly by IAU 2012 Resolution B2 [citation]. We fix the inner boundary as the nominal solar radius,

rRN,r_\odot \equiv R_{\odot}^{\mathrm{N}},
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r_\odot \equiv R_{\odot}^{\mathrm{N}},

recommended as a standard conversion constant by IAU 2015 Resolution B3 [citation]. The associated dimensionless window ratio is

xrr=RNau,x\equiv \frac{r_\odot}{r_\oplus}=\frac{R_{\odot}^{\mathrm{N}}}{\mathrm{au}},
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x\equiv \frac{r_\odot}{r_\oplus}=\frac{R_{\odot}^{\mathrm{N}}}{\mathrm{au}},

consistent with reference. The symbol rr_\odotr_\odot marks the domain boundary of the Solar-System propagation segment; it is not a fit parameter and is not adjusted in the inference below.

definition: Admissible solar-window convexity (Herglotz monotonicity). We call the declared Solar-System profile admissible on the window [r,r][r_\odot,r_\oplus][r_\odot,r_\oplus] if

ddr(rκ(r))>0for all r[r,r].\frac{d}{dr}\left(\frac{r}{\kappa(r)}\right)>0 \qquad\text{for all } r\in[r_\odot,r_\oplus].
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\frac{d}{dr}\left(\frac{r}{\kappa(r)}\right)>0
\qquad\text{for all } r\in[r_\odot,r_\oplus].

Equivalently, for the effective refractive index n(r)1/κ(r)n(r)\propto 1/\kappa(r)n(r)\propto 1/\kappa(r), one has ddr(rn(r))>0\frac{d}{dr}(r n(r))>0\frac{d}{dr}(r n(r))>0, the radial Herglotz condition used in travel-time tomography [citation]. Within the declared radial-isotropic class, this is the monotonicity condition under which the travel-time profile is Abel-invertible.

lemma: No-new-scale lemma for the inner boundary. Within the scale-free Solar-System premise adopted in Sec. reference, allowing the inner boundary rr_\odotr_\odot to vary would introduce an additional adjustable scale and would destroy the uniqueness of the forward prediction reference--reference. Therefore rr_\odotr_\odot is fixed by external convention as in Definition reference.

proof. The closed-form path factor F(q)F(q)F(q) depends on the dimensionless ratio x=r/rx=r_\odot/r_\oplusx=r_\odot/r_\oplus through reference. Since the forward relation reference depends on F(q)F(q)F(q), freedom in xxx would allow the predicted D0D_0D_0 to be shifted by moving the inner boundary. This constitutes an extra scale beyond the scale-free premise used to fix qqq (Proposition reference). Fixing rr_\odotr_\odot as a standard nominal constant removes this degree of freedom and makes the forward prediction unique.

For a radial path from rr_\odotr_\odot to rr_\oplusr_\oplus,

tprop=rrdrv(r)=1Vrrdrκ(r).t_{\mathrm{prop}} =\int_{r_\odot}^{r_\oplus}\frac{dr}{v(r)} =\frac{1}{V}\int_{r_\odot}^{r_\oplus}\frac{dr}{\kappa(r)}.
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t_{\mathrm{prop}}
=\int_{r_\odot}^{r_\oplus}\frac{dr}{v(r)}
=\frac{1}{V}\int_{r_\odot}^{r_\oplus}\frac{dr}{\kappa(r)}.

definition: Path-harmonic Earth-unit path-normalization readout. Define the Earth-unit path-normalization readout

cLtprop=Vκpath,κpathLrrdr/κ(r),Lrr.c_\oplus \equiv \frac{L}{t_{\mathrm{prop}}}=V\,\kappa_{\mathrm{path}}, \quad \kappa_{\mathrm{path}}\equiv\frac{L}{\displaystyle\int_{r_\odot}^{r_\oplus} dr/\kappa(r)}, \quad L\equiv r_\oplus-r_\odot.
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c_\oplus \equiv \frac{L}{t_{\mathrm{prop}}}=V\,\kappa_{\mathrm{path}}, 

\quad \kappa_{\mathrm{path}}\equiv\frac{L}{\displaystyle\int_{r_\odot}^{r_\oplus} dr/\kappa(r)}, 

\quad L\equiv r_\oplus-r_\odot.

lemma: Uniqueness of the harmonic mean for additive travel time. If a travel time accumulates additively along a path, tprop=0Ld/v()t_{\mathrm{prop}}=\int_0^{L} d\ell/v(\ell)t_{\mathrm{prop}}=\int_0^{L} d\ell/v(\ell), then the unique path-average calibration-rate variable consistent with L=vˉtpropL=\bar v\, t_{\mathrm{prop}}L=\bar v\, t_{\mathrm{prop}} is the harmonic mean:

vˉ  =  Ltprop  =  (1L0Ldv())1.\bar v \;=\;\frac{L}{t_{\mathrm{prop}}} \;=\;\left(\frac{1}{L}\int_0^{L}\frac{d\ell}{v(\ell)}\right)^{-1}.
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\bar v \;=\;\frac{L}{t_{\mathrm{prop}}}
\;=\;\left(\frac{1}{L}\int_0^{L}\frac{d\ell}{v(\ell)}\right)^{-1}.

proof. The relation L=vˉtpropL=\bar v\,t_{\mathrm{prop}}L=\bar v\,t_{\mathrm{prop}} determines vˉ=L/tprop\bar v=L/t_{\mathrm{prop}}\bar v=L/t_{\mathrm{prop}}. With additive travel time

tprop=0Ldv(),t_{\mathrm{prop}}=\int_0^L \frac{d\ell}{v(\ell)},
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t_{\mathrm{prop}}=\int_0^L \frac{d\ell}{v(\ell)},

substitution gives

vˉ=Ltprop=(1L0Ldv())1.\bar v = \frac{L}{t_{\mathrm{prop}}} = \left(\frac{1}{L}\int_0^L\frac{d\ell}{v(\ell)}\right)^{-1}.
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\bar v
=
\frac{L}{t_{\mathrm{prop}}}
=
\left(\frac{1}{L}\int_0^L\frac{d\ell}{v(\ell)}\right)^{-1}.

No other path-average calibration-rate variable is compatible with both additive travel time and the defining relation L=vˉtpropL=\bar v\,t_{\mathrm{prop}}L=\bar v\,t_{\mathrm{prop}}.

definition: DSN phase-count and Doppler observables. Fix a declared DSN tracking link (one-way, two-way, or three-way; coherent or non-coherent as declared) and a user specified count time TcT_cT_c. Let Pobs(Tc)P_{\mathrm{obs}}(T_c)P_{\mathrm{obs}}(T_c) denote the total-count phase observable, i.e.\ the cumulative number of counted cycles over TcT_cT_c in the corresponding DSN Doppler/phase-count data type. The DSN Doppler observable is the corresponding average cycle-rate

DobsPobs(Tc)Tc(cycles/s),D_{\mathrm{obs}}\equiv \frac{P_{\mathrm{obs}}(T_c)}{T_c}\quad (\mathrm{cycles/s}),
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D_{\mathrm{obs}}\equiv \frac{P_{\mathrm{obs}}(T_c)}{T_c}\quad (\mathrm{cycles/s}),

and is recorded together with range and ancillary identification metadata (station IDs, band, count time, ramp and turnaround information) in standard navigation data products [citation].

definition: Observed/computed pairing and minimal computed model. Navigation data analysis is performed on paired observed and computed values for the same DSN data type and the same count interval [citation]. For a declared datum, let Pcmp[M](Tc)P_{\mathrm{cmp}}[\mathcal{M}](T_c)P_{\mathrm{cmp}}[\mathcal{M}](T_c) denote the computed total-count phase (cycles) produced by a declared model M\mathcal{M}\mathcal{M} (trajectory, station geometry, media corrections, and RF-system information), and define the computed reference as

P0(Tc)Pcmp[Mmin](Tc)(cycles).P_{0}(T_c)\equiv P_{\mathrm{cmp}}[\mathcal{M}_{\min}](T_c)\quad (\mathrm{cycles}).
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P_{0}(T_c)\equiv P_{\mathrm{cmp}}[\mathcal{M}_{\min}](T_c)\quad (\mathrm{cycles}).

Here Mmin\mathcal{M}_{\min}\mathcal{M}_{\min} is a minimal computed model specification: the smallest declared model for which the computed phase-count is unambiguous and comparable to Pobs(Tc)P_{\mathrm{obs}}(T_c)P_{\mathrm{obs}}(T_c). Concretely, Mmin\mathcal{M}_{\min}\mathcal{M}_{\min} must specify, at minimum,

- the DSN data type and link multiplicity (one-way/two-way/three-way) and whether the link is coherent or non-coherent; - the count interval TcT_cT_c (and the time tags defining its endpoints); - the frequency plan used by the DSN for that interval, including any ramp table and the spacecraft transponder turnaround ratio [citation]; - the reference trajectory/geometry used to compute light-time along the signal path (including the participating stations for three-way links) together with the declared light-time model terms used in the computed observable; - any additional hardware/time-scale delays and calibration terms that are part of the DSN data type definition for the chosen observable (e.g.\ transponder delay, station delays, time-scale conversions) [citation]; - the declared set of propagation and media corrections used in the computed observable (e.g.\ troposphere, ionosphere, solar plasma), or an explicit declaration that a given correction is not applied.

If any required element is missing or ambiguous for a given pass, then P0P_{0}P_{0} is not well-defined for that pass and the pass is excluded from Φ\Phi\Phi-based inference.

definition: Admissible phase-count segment. A tracking pass (or sub-arc) is admissible for estimating Φ\Phi\Phi and testing the scale-free signature if it satisfies both:

- Model specification: the minimal computed model Mmin\mathcal{M}_{\min}\mathcal{M}_{\min} in Definition reference is satisfied for the pass, so that (Pobs,P0)(P_{\mathrm{obs}},P_{0})(P_{\mathrm{obs}},P_{0}) is an observed/computed pair for the same DSN data type and count interval; - Solar-plasma gate: the Sun--Probe--Earth (SPE) angle is sufficiently large that unmodeled solar-plasma effects cannot masquerade as a curvature-layering signature on the phase count. The DSN Services Catalog notes that tracking accuracy degrades for SPE angles below 1010^\circ10^\circ, and that S-band data are generally unusable below 55^\circ5^\circ [citation]. Accordingly, a conservative admissibility rule is adopted: we exclude the near-conjunction regime SPE<5\mathrm{SPE}<5^\circ\mathrm{SPE}<5^\circ for all inferences, and unless an explicit dual-frequency or validated solar-plasma calibration is declared as part of Mmin\mathcal{M}_{\min}\mathcal{M}_{\min} we require SPE10\mathrm{SPE}\ge 10^\circ\mathrm{SPE}\ge 10^\circ [citation]. If a calibration is available, an extended analysis may relax the SPE10\mathrm{SPE}\ge 10^\circ\mathrm{SPE}\ge 10^\circ rule while keeping the SPE<5\mathrm{SPE}<5^\circ\mathrm{SPE}<5^\circ exclusion [citation].

This gate prevents the Solar-System domain boundary (Definition reference) from being effectively replaced by a variable cutoff set by conjunction-dependent plasma contamination.

lemma: Functorial count structure of coherent total-count phase. Fix a declared coherent DSN data type and a phase-continuous tracking pass. Let IPobs(I)I\mapsto P_{\mathrm{obs}}(I)I\mapsto P_{\mathrm{obs}}(I) denote the observed total-count phase on declared reception intervals III within that pass. Then:

- if I=I1I2I=I_1\sqcup I_2I=I_1\sqcup I_2 is a disjoint union of contiguous subintervals within the same phase-continuous pass, then

Pobs(I)=Pobs(I1)+Pobs(I2);P_{\mathrm{obs}}(I)=P_{\mathrm{obs}}(I_1)+P_{\mathrm{obs}}(I_2);
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P_{\mathrm{obs}}(I)=P_{\mathrm{obs}}(I_1)+P_{\mathrm{obs}}(I_2);

- the same additivity holds for the computed reference P0(I)P_{0}(I)P_{0}(I) when the observed/computed pairing is declared for the same DSN data type, count interval, frequency plan, and coherent turnaround rule; - repeated subdivision and recombination of a declared interval leaves the total count unchanged.

Hence coherent total-count phase defines a finitely additive, refinement-stable interval functional on declared count intervals.

proof. By Definition reference, total-count phase is a cumulative cycle count on a user-specified count interval. In standard DSN processing, such counts are meaningful only across subintervals on which the counted phase is continuous, and observed/computed values are paired for the same DSN data type and count interval under a fixed frequency plan and, for coherent links, a fixed transponder turnaround ratio [citation]. Concatenating contiguous phase-continuous subintervals therefore concatenates their counted cycles, giving additivity for both observed and computed counts. Since the count on a union is the sum on its pieces, further subdivision changes only the bookkeeping, not the total accumulated count.

lemma: Cycle count and range change over a count interval. A DSN Doppler/phase-count observable is a counted carrier phase-difference measurement; each counted cycle corresponds to one effective carrier wavelength of accumulated phase-path change in the declared observable [citation]. Therefore the total-count phase Pobs(Tc)P_{\mathrm{obs}}(T_c)P_{\mathrm{obs}}(T_c) provides a direct measure of propagation-distance change over TcT_cT_c:

ΔL(Tc)=λeffPobs(Tc),\Delta \mathcal{L}(T_c)=\lambda_{\mathrm{eff}}\,P_{\mathrm{obs}}(T_c),
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\Delta \mathcal{L}(T_c)=\lambda_{\mathrm{eff}}\,P_{\mathrm{obs}}(T_c),

where λeff\lambda_{\mathrm{eff}}\lambda_{\mathrm{eff}} is the effective carrier wavelength determined by the declared frequency plan (including turnaround and ramp information) already contained in Mmin\mathcal{M}_{\min}\mathcal{M}_{\min} (Definition reference) [citation]. The corresponding one-way range change satisfies

ΔR(Tc)=λeffχPobs(Tc),\Delta R(T_c)=\frac{\lambda_{\mathrm{eff}}}{\chi}\,P_{\mathrm{obs}}(T_c),
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\Delta R(T_c)=\frac{\lambda_{\mathrm{eff}}}{\chi}\,P_{\mathrm{obs}}(T_c),

where χ\chi\chi is a fixed link multiplicity factor (χ=1\chi=1\chi=1 for one-way, χ=2\chi=2\chi=2 for two-way and three-way coherent links) [citation]. Since χ\chi\chi is fixed by the declared DSN data type, it cannot be tuned to absorb an rrr-scaling signature used in Sec. reference.

Figure or table content is omitted from the web reader; use the canonical manuscript for the exact object.

definition: Frequency-free dimensionless layered path functional. For a declared propagation segment γ\gamma\gamma of Euclidean length LγγdL_\gamma\equiv\int_\gamma d\ellL_\gamma\equiv\int_\gamma d\ell, define the propagation time

tprop(γ)=γdv()=1Vγdκ().t_{\mathrm{prop}}(\gamma)=\int_{\gamma}\frac{d\ell}{v(\ell)} =\frac{1}{V}\int_{\gamma}\frac{d\ell}{\kappa(\ell)}.
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t_{\mathrm{prop}}(\gamma)=\int_{\gamma}\frac{d\ell}{v(\ell)}
 =\frac{1}{V}\int_{\gamma}\frac{d\ell}{\kappa(\ell)}.

Define the unlayered reference travel time for the same segment by the model restriction κ()1\kappa(\ell)\equiv 1\kappa(\ell)\equiv 1:

t0(γ)tprop(γ)κ1=LγV.t_{0}(\gamma)\equiv t_{\mathrm{prop}}(\gamma)\big|_{\kappa\equiv 1}=\frac{L_\gamma}{V}.
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t_{0}(\gamma)\equiv t_{\mathrm{prop}}(\gamma)\big|_{\kappa\equiv 1}=\frac{L_\gamma}{V}.

For an admissible DSN phase-count pass (Definition reference) let Pobs(γ)P_{\mathrm{obs}}(\gamma)P_{\mathrm{obs}}(\gamma) denote the observed total-count phase (cycles) on γ\gamma\gamma and let P0(γ)P_{0}(\gamma)P_{0}(\gamma) denote the corresponding computed reference count produced by Mmin\mathcal{M}_{\min}\mathcal{M}_{\min} (Definition reference) for the same DSN data type and count interval. The frequency-free, dimensionless phase-ratio functional is

Φ(γ)Pobs(γ)P0(γ).\Phi(\gamma)\equiv \frac{P_{\mathrm{obs}}(\gamma)}{P_{0}(\gamma)}.
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\Phi(\gamma)\equiv \frac{P_{\mathrm{obs}}(\gamma)}{P_{0}(\gamma)}.

Under the matched observed/computed pairing and count-interval contract fixed by Definitions reference and reference, Lemma reference shows that on admissible coherent, non-dispersive segments the operational ratio Φ\Phi\Phi is the quotient of two coherent count measures over the same declared interval algebra and, absent any extra admissible channel, is forced to factor through the elapsed-time quotient of the declared segment. In particular, for the Solar-System reference path in reference it yields the dimensionless path-normalization readout Vread/c=ΦV_{\rm read}/c_\oplus=\PhiV_{\rm read}/c_\oplus=\Phi by Lemma reference. The observed-minus-computed residual in cycles is PobsP0=(Φ1)P0P_{\mathrm{obs}}-P_{0}=(\Phi-1)\,P_{0}P_{\mathrm{obs}}-P_{0}=(\Phi-1)\,P_{0}, so Φ1\Phi-1\Phi-1 is the natural dimensionless residual used to test the layered signature against DSN computed observables [citation].

definition: Declared operational interpretation package. We say that a DSN-calibrated inference instance satisfies the declared operational interpretation package if all of the following hold:

- Declared data type and count interval: the link definition, data type, band, and count interval are declared as in Definition reference; - Observed/computed pairing: the computed reference P0P_{0}P_{0} is generated as P0=Pcmp[Mmin]P_{0}=P_{\mathrm{cmp}}[\mathcal{M}_{\min}]P_{0}=P_{\mathrm{cmp}}[\mathcal{M}_{\min}] under the minimal computed model contract in Definition reference, so that observed and computed values refer to the same DSN data type and count interval [citation]; - Admissibility condition: the pass satisfies the admissibility criteria of Definition reference; - Primary inference channel and control comparison: primary inference is performed on coherent two-way/three-way links (F2/F3), while one-way non-coherent links (F1) are retained as a control comparison for oscillator/clock contamination [citation]; - Dispersive-media classification when multi-band is available: if the same declared segment is observed at two or more downlink carrier frequencies, apply the dispersive scaling test in Definition reference; passes classified as dispersive are excluded from curvature-layering inference unless a validated dispersive calibration is explicitly declared as part of Mmin\mathcal{M}_{\min}\mathcal{M}_{\min} (Definition reference). - Cross-channel consistency when external witnesses are available: if admissible angular/lens data or admissible clock-transfer data exist for the same boundary-normalized Solar-System window, they are used as external witness channels and must be consistent with the κ(r)\kappa(r)\kappa(r) reconstructed from the delay channel in the sense formalized in Definition reference. If the clock witness is available on a closed comparison network, the loop-exactness condition in Definition reference is imposed in addition. Otherwise the shared-map identification reference is rejected for that window. - Declared π\pi\pi-normalization class: for the present class-bound readout, the normalization is performed on the coherent, non-dispersive admissible reparameterization class of the radial Solar-System segment from rr_\odotr_\odot to rr_\oplusr_\oplus underlying reference. We denote this class by Γπ\Gamma_{\pi}\Gamma_{\pi} and its reference representative by γref\gamma_{\mathrm{ref}}\gamma_{\mathrm{ref}}. This clause introduces no additional geometric scale beyond the segment already fixed by reference; the class-bound readout property used below is established in Lemma reference.

definition: Three-channel acceptance criterion for the shared map. Fix the same Solar-System window, the same boundary normalization, and the same admissibility rules. Let κdelay(r)\kappa_{\mathrm{delay}}(r)\kappa_{\mathrm{delay}}(r) denote the profile reconstructed from admissible line-of-sight delay/range data. If admissible angular/lens data can be reduced to a boundary-normalized witness profile κangle(r)\kappa_{\mathrm{angle}}(r)\kappa_{\mathrm{angle}}(r) on that window, then it must agree with κdelay(r)\kappa_{\mathrm{delay}}(r)\kappa_{\mathrm{delay}}(r). If admissible clock-rate transfer or redshift data can be reduced to a boundary-normalized witness profile κclock(r)\kappa_{\mathrm{clock}}(r)\kappa_{\mathrm{clock}}(r), then it too must agree with κdelay(r)\kappa_{\mathrm{delay}}(r)\kappa_{\mathrm{delay}}(r). In the fully witnessed case, where both witness profiles are available, the acceptance criterion becomes

κdelay(r)=κangle(r)=κclock(r)for r[r,r].\kappa_{\mathrm{delay}}(r)=\kappa_{\mathrm{angle}}(r)=\kappa_{\mathrm{clock}}(r) \qquad \text{for } r\in[r_\odot,r_\oplus].
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\kappa_{\mathrm{delay}}(r)=\kappa_{\mathrm{angle}}(r)=\kappa_{\mathrm{clock}}(r)
\qquad \text{for } r\in[r_\odot,r_\oplus].

When the clock witness is available on a closed comparison network, this agreement requirement is supplemented by the loop-exactness condition in Definition reference. Any failure of reference, of the corresponding pairwise agreement when only one witness channel is available, or of the applicable loop-exactness condition falsifies the shared-map identification rather than redefining κ\kappa\kappa.

definition: Clock-loop exactness on closed comparison networks. Suppose admissible clock-transfer or redshift data are available on a closed comparison network for the same stationary or quasi-stationary Solar-System window. Let RijR_{ij}R_{ij} denote the boundary-normalized frequency ratio assigned to the oriented edge iji\to ji\to j under the declared transfer reduction. The clock witness is called loop-exact if for every closed loop L=(i1i2imi1)\mathcal L=(i_1\to i_2\to\cdots\to i_m\to i_1)\mathcal L=(i_1\to i_2\to\cdots\to i_m\to i_1),

a=1mRiaia+1=1,im+1i1.\prod_{a=1}^{m} R_{i_a i_{a+1}} =1,\qquad i_{m+1}\equiv i_1.
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\prod_{a=1}^{m} R_{i_a i_{a+1}} =1,\qquad i_{m+1}\equiv i_1.

Equivalently, LlnRij=0\sum_{\mathcal L}\ln R_{ij}=0\sum_{\mathcal L}\ln R_{ij}=0. Under the shared-map identification this is the operational no-holonomy condition Ldlnκ=0\oint_{\mathcal L} d\ln\kappa =0\oint_{\mathcal L} d\ln\kappa =0. Failure of reference rejects the shared map on that window.

remark: Logical status of the three-channel criterion. Definition reference and Definition reference are admissibility rules. Here κdelay\kappa_{\mathrm{delay}}\kappa_{\mathrm{delay}} is constructed operationally from DSN-style delay/range observables, κangle\kappa_{\mathrm{angle}}\kappa_{\mathrm{angle}} enters as an external uniqueness witness within the declared radial-isotropic class, and κclock\kappa_{\mathrm{clock}}\kappa_{\mathrm{clock}} enters as a single-geometry equality test and falsifier. On stationary or quasi-stationary windows, the clock witness may additionally be checked by loop exactness of reduced frequency ratios, reflecting the exact redshift-potential picture expected for standard clocks [citation]. The angular and clock channels therefore remain external witnesses of unequal status relative to the internal delay derivation.

definition: Multi-band dispersive scaling test (plasma classification). Let γ\gamma\gamma be an admissible segment and let ρ(f)Φ(γ;f)1\rho(f)\equiv \Phi(\gamma;f)-1\rho(f)\equiv \Phi(\gamma;f)-1 denote the dimensionless observed-minus-computed phase ratio residual obtained from the same declared DSN data type and count interval at downlink carrier frequency fff. If two or more bands are available for the same geometry and the residual family is consistent (within measurement uncertainty and within the declared computed model) with the dispersive scaling law

ρ(f)  1f2,\rho(f)\ \propto\ \frac{1}{f^{2}},
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\rho(f)\ \propto\ \frac{1}{f^{2}},

equivalently ρ(fi)fi2\rho(f_i)f_i^{2}\rho(f_i)f_i^{2} is constant across bands, then the residual is classified as dispersive (media-dominated) rather than curvature-layering dominated. Such 1/f21/f^{2}1/f^{2} scaling is a characteristic signature of plasma dispersion in deep-space radiometric observables and appears explicitly in standard error models [citation]. Under Contract C\mathsf{C}\mathsf{C}, dispersive-classified passes are excluded from curvature-layering inference unless a validated dispersive calibration is explicitly declared in Mmin\mathcal{M}_{\min}\mathcal{M}_{\min} (Definition reference) [citation].

lemma: Coherent count-measure quotient representation and no-extra-channel theorem under Contract C\mathsf{C}\mathsf{C}. Assume Contract C\mathsf{C}\mathsf{C} (Definition reference) and the CHC shared map reference. Let γ\gamma\gamma be an admissible coherent DSN phase-count segment for which Pobs(γ)P_{\mathrm{obs}}(\gamma)P_{\mathrm{obs}}(\gamma) and P0(γ)P_{0}(\gamma)P_{0}(\gamma) are paired observed/computed total-count phase observables of the same DSN data type, count interval, frequency plan, and turnaround ratio. Let Iγ\mathfrak I_\gamma\mathfrak I_\gamma denote the algebra of declared reception subintervals of a phase-continuous pass realizing γ\gamma\gamma, and define

μobs(I)Pobs(I),μ0(I)P0(I),IIγ.\mu_{\mathrm{obs}}(I)\equiv P_{\mathrm{obs}}(I),\qquad \mu_{0}(I)\equiv P_{0}(I),\qquad I\in\mathfrak I_\gamma.
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\mu_{\mathrm{obs}}(I)\equiv P_{\mathrm{obs}}(I),\qquad
\mu_{0}(I)\equiv P_{0}(I),\qquad I\in\mathfrak I_\gamma.

Assume further that: (i) μobs\mu_{\mathrm{obs}}\mu_{\mathrm{obs}} and μ0\mu_0\mu_0 satisfy the functoriality of Lemma reference; (ii) both are locally absolutely continuous with respect to reception time on phase-continuous passes; and (iii) after the dispersive rejection of Definition reference, no residual band label remains. Then the coherent observable quotient is representable only as a quotient of two count measures over the same declared interval algebra, and any curvature-layering contribution consistent with the matched observed/computed contract must factor through the same elapsed-time measure of the declared segment. Consequently

Φ(γ)=Pobs(γ)P0(γ)=μobs(γ)μ0(γ)=tprop(γ)t0(γ)=1Lγγdκ().\Phi(\gamma)=\frac{P_{\mathrm{obs}}(\gamma)}{P_{0}(\gamma)} =\frac{\mu_{\mathrm{obs}}(\gamma)}{\mu_0(\gamma)} =\frac{t_{\mathrm{prop}}(\gamma)}{t_{0}(\gamma)} =\frac{1}{L_\gamma}\int_{\gamma}\frac{d\ell}{\kappa(\ell)}.
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\Phi(\gamma)=\frac{P_{\mathrm{obs}}(\gamma)}{P_{0}(\gamma)}
=\frac{\mu_{\mathrm{obs}}(\gamma)}{\mu_0(\gamma)}
=\frac{t_{\mathrm{prop}}(\gamma)}{t_{0}(\gamma)}
=\frac{1}{L_\gamma}\int_{\gamma}\frac{d\ell}{\kappa(\ell)}.

Moreover, any additional channel affecting Φ\Phi\Phi without appearing in the same elapsed-time functional would violate at least one of: finite count additivity, coherent observed/computed pairing, band-independence after dispersive rejection, or refinement stability on declared intervals.

proof. By Lemma reference, the coherent total-count phase defines a finitely additive, refinement-stable interval functional on the declared interval algebra Iγ\mathfrak I_\gamma\mathfrak I_\gamma. By local absolute continuity with respect to reception time, there exist local count densities such that

dμobs=λobs(t)dt,dμ0=λ0(t)dt.d\mu_{\mathrm{obs}}=\lambda_{\mathrm{obs}}(t)\,dt, \qquad d\mu_{0}=\lambda_{0}(t)\,dt.
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d\mu_{\mathrm{obs}}=\lambda_{\mathrm{obs}}(t)\,dt,
\qquad
d\mu_{0}=\lambda_{0}(t)\,dt.

Under the matched observed/computed contract, the carrier scale, count-unit conventions, coherent turnaround rule, and declared DSN data type are fixed multiplicative ingredients of both measures; after the dispersive rejection of Definition reference, no independent band label remains. Hence the only admissible observable quotient is the quotient of two coherent count measures over the same interval algebra. Under the CHC shared map reference, the only declared local scalar distortion channel available to such a quotient is the elapsed-time density

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03

Scale-free Solar-System layering and the path factor

Power-law profile and closed-form path factorFixing \(q=3/4\) from a scale-free invariant (and a no-go)Fixing q=3/4 from a scale-free invariant (and a no-go)

Power-law profile and closed-form path factor Assume a scale-free Solar-System window (rrrr_\odot\ll r\lesssim r_\oplusr_\odot\ll r\lesssim r_\oplus) in the local self-similarity sense: there exists an open interval B(0,)\mathcal{B}\subset(0,\infty)\mathcal{B}\subset(0,\infty) containing 111 such that for any scale factor bBb\in\mathcal{B}b\in\mathcal{B} for which both rrr and brbrbr remain within the window, the layering profile obeys

κ(br)=G(b)κ(r),\kappa(br)=G(b)\,\kappa(r),
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\kappa(br)=G(b)\,\kappa(r),

for some positive function GGG that depends only on the scale factor. Under mild regularity (differentiability in rrr and differentiability of GGG at b=1b=1b=1), this local condition is enough to force a power-law profile [citation]:

lemma: Local self-similarity implies a power-law profile. Assume κ:(0,)(0,)\kappa:(0,\infty)\to(0,\infty)\kappa:(0,\infty)\to(0,\infty) is differentiable on the scale-free window and satisfies reference for all bBb\in\mathcal{B}b\in\mathcal{B} with 1B1\in\mathcal{B}1\in\mathcal{B}, where GGG is differentiable at b=1b=1b=1. Then there exists an exponent qRq\in\mathbb{R}q\in\mathbb{R} such that G(1)=1G(1)=1G(1)=1, q=G(1)q=G'(1)q=G'(1), and

κ(r)=κ(r)(rr)q\kappa(r)=\kappa(r_\oplus)\left(\frac{r}{r_\oplus}\right)^q
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\kappa(r)=\kappa(r_\oplus)\left(\frac{r}{r_\oplus}\right)^q

on the window.

proof. Setting b=1b=1b=1 in reference gives G(1)=1G(1)=1G(1)=1. Taking natural logs yields

lnκ(br)lnκ(r)=lnG(b).\ln\kappa(br)-\ln\kappa(r)=\ln G(b).
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\ln\kappa(br)-\ln\kappa(r)=\ln G(b).

Differentiate with respect to bbb at b=1b=1b=1 (for fixed rrr). Since κ\kappa\kappa is differentiable,

ddblnκ(br)b=1=rκ(r)κ(r),\left.\frac{d}{db}\ln\kappa(br)\right|_{b=1}=\frac{r\,\kappa'(r)}{\kappa(r)},
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\left.\frac{d}{db}\ln\kappa(br)\right|_{b=1}=\frac{r\,\kappa'(r)}{\kappa(r)},

and since G(1)=1G(1)=1G(1)=1 and GGG is differentiable at b=1b=1b=1,

ddblnG(b)b=1=G(1)=q.\left.\frac{d}{db}\ln G(b)\right|_{b=1}=G'(1)=q.
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\left.\frac{d}{db}\ln G(b)\right|_{b=1}=G'(1)=q.

Therefore rκ(r)/κ(r)=qr\,\kappa'(r)/\kappa(r)=qr\,\kappa'(r)/\kappa(r)=q, i.e.\ d(lnκ)/d(lnr)=qd(\ln\kappa)/d(\ln r)=qd(\ln\kappa)/d(\ln r)=q on the window. Integrating gives lnκ(r)=qlnr+C\ln\kappa(r)=q\ln r + C\ln\kappa(r)=q\ln r + C, hence κ(r)=Crq\kappa(r)=C' r^q\kappa(r)=C' r^q. Evaluating at r=rr=r_\oplusr=r_\oplus fixes C=κ(r)rqC'=\kappa(r_\oplus)r_\oplus^{-q}C'=\kappa(r_\oplus)r_\oplus^{-q}, yielding reference.

Thus the minimal family consistent with scale-freeness is the power-law profile

κ(r)=κ(rr)q,q0,κκ(r).\kappa(r)=\kappa_\oplus\left(\frac{r}{r_\oplus}\right)^q,\qquad q\ge 0,\qquad \kappa_\oplus\equiv \kappa(r_\oplus).
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\kappa(r)=\kappa_\oplus\left(\frac{r}{r_\oplus}\right)^q,\qquad q\ge 0,\qquad \kappa_\oplus\equiv \kappa(r_\oplus).

Let au\mathrm{au}\mathrm{au} denote the astronomical unit, defined as exactly 149597870700149\,597\,870\,700149\,597\,870\,700 m by IAU 2012 Resolution B2 [citation], and let RN695700000R_{\odot}^{\mathrm{N}}\equiv 695\,700\,000R_{\odot}^{\mathrm{N}}\equiv 695\,700\,000 m denote the nominal solar radius recommended by IAU 2015 Resolution B3 [citation]. Define the dimensionless window ratio

xRNau.x\equiv \frac{R_{\odot}^{\mathrm{N}}}{\mathrm{au}}.
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x\equiv \frac{R_{\odot}^{\mathrm{N}}}{\mathrm{au}}.

lemma: Closed form for the path factor. For q1q\neq 1q\neq 1, inserting reference into reference yields

κpath=κF(q),F(q)(1q)(1x)1x1q.\kappa_{\mathrm{path}}=\kappa_\oplus\,F(q), \qquad F(q)\equiv\frac{(1-q)(1-x)}{1-x^{1-q}}.
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\kappa_{\mathrm{path}}=\kappa_\oplus\,F(q),
\qquad
F(q)\equiv\frac{(1-q)(1-x)}{1-x^{1-q}}.

Fixing q=3/4q=3/4q=3/4 from a scale-free invariant (and a no-go)Fixing q=3/4 from a scale-free invariant (and a no-go)

proposition: Premise-fixed 3+1 shell-extensivity selects q=3/4q=3/4q=3/4 on the declared scale-free window. Assume the shared distortion map reference so that both spatial propagation scales and local clock scales are reduced by the same factor κ(r)\kappa(r)\kappa(r). In a scale-free Solar-System window, require that no additional dimensionful scale beyond rrr enters the layering profile. Let α\alpha\alpha denote the a priori unknown self-similarity exponent of the local scaling action in Lemma reference. Require further that the orbit label for adjacent radial shells be extensive under shell concatenation. For one shared time dimension and ddd spatial dimensions, the corresponding shell-content candidate is

I(r)κ(r)d+1(r/r)d.\mathcal{I}(r)\equiv \frac{\kappa(r)^{d+1}}{(r/r_\oplus)^{d}}.
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\mathcal{I}(r)\equiv \frac{\kappa(r)^{d+1}}{(r/r_\oplus)^{d}}.

Require this shell-content candidate to be invariant across the window. Then

(d+1)αd=0.(d+1)\alpha-d=0.
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(d+1)\alpha-d=0.

Under the power-law ansatz reference, the self-similarity exponent equals qqq, and therefore

q=dd+1.q=\frac{d}{d+1}.
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q=\frac{d}{d+1}.

For d=3d=3d=3 this yields

q=34.q=\frac{3}{4}.
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q=\frac{3}{4}.

proof. By the stated shell-extensivity premise, the orbit label must compose consistently across adjacent radial shells. Because the shared map carries one time dimension and ddd spatial dimensions through the same scalar κ\kappa\kappa, the shell-content candidate reference is the monomial orbit label compatible with that 3+1 shell valuation. By Lemma reference, this candidate is invariant under the general scaling action reference if and only if (d+1)αd=0(d+1)\alpha-d=0(d+1)\alpha-d=0, which gives reference. Under the power-law ansatz, κ(br)=bqκ(r)\kappa(br)=b^{q}\kappa(r)\kappa(br)=b^{q}\kappa(r), so the self-similarity exponent equals q=αq=\alphaq=\alpha. Hence reference and reference.

remark: Why the invariant uses κd+1\kappa^{d+1}\kappa^{d+1} and (r/r)d(r/r_\oplus)^d(r/r_\oplus)^d. Under the shared distortion map reference, the same dimensionless profile κ(r)\kappa(r)\kappa(r) rescales the local time unit (dτ=κdTd\tau=\kappa\,dTd\tau=\kappa\,dT) and the calibration-layer path-normalization variable (v=Vκv=V\kappav=V\kappa). Hence a single κ\kappa\kappa acts as a common scale factor on one time dimension and on the ddd spatial dimensions of an isotropic organizer, so the natural isotropic (time+space) monomial scale factor is κd+1\kappa^{d+1}\kappa^{d+1}. In a scale-free Solar-System window, rrr (measured in Earth units r/rr/r_\oplusr/r_\oplus) is the only available length scale. If, in addition, the orbit label for adjacent radial shells is required to compose extensively under shell concatenation, then the monomial shell-content candidate is (r/r)dκd+1(r/r_\oplus)^{-d}\kappa^{d+1}(r/r_\oplus)^{-d}\kappa^{d+1}. Requiring the ratio I(r)=κ(r)d+1/(r/r)d\mathcal{I}(r)=\kappa(r)^{d+1}/(r/r_\oplus)^d\mathcal{I}(r)=\kappa(r)^{d+1}/(r/r_\oplus)^d to be constant is therefore the strongest shell-extensive statement available within the stated 3+1 shared-map premises. Equivalently, the local self-similarity relation reference defines a scaling group acting on profiles (r,κ(r))(r,\kappa(r))(r,\kappa(r)). In this setting, I(r)\mathcal{I}(r)\mathcal{I}(r) acts as a maximal invariant for the induced action on the pair (r,κ)(r,\kappa)(r,\kappa): any scale-free invariant scalar factors through I\mathcal{I}\mathcal{I} [citation]. In particular, once one common distortion scalar κ\kappa\kappa carries one time dimension and ddd spatial dimensions, the shell-content index I(r)=κ(r)d+1/(r/r)d\mathcal{I}(r)=\kappa(r)^{d+1}/(r/r_\oplus)^d\mathcal{I}(r)=\kappa(r)^{d+1}/(r/r_\oplus)^d is the shell-content candidate selected by the stated 3+1 extensivity premise; Lemma reference then shows that, if this candidate is required to be invariant under the general action reference, the self-similarity exponent must satisfy (d+1)αd=0(d+1)\alpha-d=0(d+1)\alpha-d=0, and under the power-law ansatz this yields q=α=d/(d+1)q=\alpha=d/(d+1)q=\alpha=d/(d+1).

lemma: General-α\alpha\alpha maximal invariant and orbit rigidity of the shell-content index. Assume the shared distortion map reference and the local self-similarity premise reference on a scale-free Solar-System window. Consider the induced one-parameter scaling action on the pair (r,κ)(r,\kappa)(r,\kappa) defined (in Earth units) by

(r,κ)  (br, bακ),b>0,(r,\kappa)\ \mapsto\ (br,\ b^{\alpha}\kappa),\qquad b>0,
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(r,\kappa)\ \mapsto\ (br,\ b^{\alpha}\kappa),\qquad b>0,

where α\alpha\alpha is a priori unknown. Then

Mα(r,κ)κ(r/r)αM_{\alpha}(r,\kappa)\equiv \frac{\kappa}{(r/r_\oplus)^{\alpha}}
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M_{\alpha}(r,\kappa)\equiv \frac{\kappa}{(r/r_\oplus)^{\alpha}}

is a maximal invariant for reference: it is invariant under the action, and two points (r1,κ1)(r_1,\kappa_1)(r_1,\kappa_1) and (r2,κ2)(r_2,\kappa_2)(r_2,\kappa_2) lie on the same orbit if and only if Mα(r1,κ1)=Mα(r2,κ2)M_{\alpha}(r_1,\kappa_1)=M_{\alpha}(r_2,\kappa_2)M_{\alpha}(r_1,\kappa_1)=M_{\alpha}(r_2,\kappa_2). Consequently any dimensionless scalar invariant of the scaling action is a function of MαM_\alphaM_\alpha [citation]. In particular, the shared-map shell-content index

I(r)=κ(r)d+1(r/r)d\mathcal{I}(r)=\frac{\kappa(r)^{d+1}}{(r/r_\oplus)^d}
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\mathcal{I}(r)=\frac{\kappa(r)^{d+1}}{(r/r_\oplus)^d}

is invariant under reference if and only if

(d+1)αd=0.(d+1)\alpha-d=0.
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(d+1)\alpha-d=0.

proof. First, reference leaves MαM_\alphaM_\alpha invariant:

bακ(br/r)α=κ(r/r)α.\frac{b^\alpha\kappa}{(br/r_\oplus)^\alpha}=\frac{\kappa}{(r/r_\oplus)^\alpha}.
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\frac{b^\alpha\kappa}{(br/r_\oplus)^\alpha}=\frac{\kappa}{(r/r_\oplus)^\alpha}.

For orbit separation, suppose (r2,κ2)=(br1,bακ1)(r_2,\kappa_2)=(br_1,b^\alpha\kappa_1)(r_2,\kappa_2)=(br_1,b^\alpha\kappa_1) for some b>0b>0b>0; then Mα(r2,κ2)=Mα(r1,κ1)M_\alpha(r_2,\kappa_2)=M_\alpha(r_1,\kappa_1)M_\alpha(r_2,\kappa_2)=M_\alpha(r_1,\kappa_1). Conversely, if

κ2(r2/r)α=κ1(r1/r)α,\frac{\kappa_2}{(r_2/r_\oplus)^\alpha}=\frac{\kappa_1}{(r_1/r_\oplus)^\alpha},
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\frac{\kappa_2}{(r_2/r_\oplus)^\alpha}=\frac{\kappa_1}{(r_1/r_\oplus)^\alpha},

then κ2=(r2/r1)ακ1\kappa_2=(r_2/r_1)^\alpha\kappa_1\kappa_2=(r_2/r_1)^\alpha\kappa_1. Taking b=r2/r1b=r_2/r_1b=r_2/r_1 yields (r2,κ2)=(br1,bακ1)(r_2,\kappa_2)=(br_1,b^\alpha\kappa_1)(r_2,\kappa_2)=(br_1,b^\alpha\kappa_1), so the points lie on the same orbit. Hence MαM_\alphaM_\alpha indexes the orbits and is maximal invariant.

Now apply the same action to the shell-content index:

I(bακ)d+1(br/r)d=b(d+1)αdκd+1(r/r)d.\mathcal{I}\mapsto \frac{(b^\alpha\kappa)^{d+1}}{(br/r_\oplus)^d} = b^{(d+1)\alpha-d}\, \frac{\kappa^{d+1}}{(r/r_\oplus)^d}.
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\mathcal{I}\mapsto
\frac{(b^\alpha\kappa)^{d+1}}{(br/r_\oplus)^d}
=
b^{(d+1)\alpha-d}\,
\frac{\kappa^{d+1}}{(r/r_\oplus)^d}.

Therefore I\mathcal{I}\mathcal{I} is invariant if and only if (d+1)αd=0(d+1)\alpha-d=0(d+1)\alpha-d=0. In particular, once the shell-content candidate reference is selected by the stated 3+1 extensivity premise, the general-α\alpha\alpha action leaves no remaining freedom in the exponent, so the fixed point is forced rather than chosen.

remark: Status of the exponent fixing. The value q=3/4q=3/4q=3/4 is fixed only within the combined premises of (i) local scale-freeness on the Solar-System window, (ii) one shared distortion scalar acting on one time and three spatial dimensions, and (iii) shell-extensivity under radial concatenation. It is not extracted here from DSN delay/range data alone. The observational role of Solar-System time-transfer is narrower: it tests whether an admissible scale-free window remains compatible with the exponent selected by those premises.

remark: No-go for qd/(d+1)q\neq d/(d+1)q\neq d/(d+1) under the stated scale-free premise. If κ(r)=κ(r/r)q\kappa(r)=\kappa_\oplus (r/r_\oplus)^q\kappa(r)=\kappa_\oplus (r/r_\oplus)^q with qd/(d+1)q\neq d/(d+1)q\neq d/(d+1), then I(r)r(d+1)qd\mathcal{I}(r)\propto r^{(d+1)q-d}\mathcal{I}(r)\propto r^{(d+1)q-d} is not constant, so the window is not scale-free in the sense of an invariant: an additional scale is implicitly introduced. The stated scale-free premise is therefore equivalent to the exponent condition.

remark: Primary falsifier for qqq. Solar-System time-transfer constraints act directly on dr/κ(r)\int dr/\kappa(r)\int dr/\kappa(r) (Sec. reference); if those constraints exclude a scale-free exponent near q=3/4q=3/4q=3/4 over the relevant window, the choice reference is falsified.

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04

Calibration identities

proposition: Declared-class Earth-ratio identity on the adopted Solar-System map. Under reference and reference,

R=1κκpath=1κ2F(q).R=\frac{1}{\kappa_\oplus\,\kappa_{\mathrm{path}}} =\frac{1}{\kappa_\oplus^2\,F(q)}.
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R=\frac{1}{\kappa_\oplus\,\kappa_{\mathrm{path}}}
=\frac{1}{\kappa_\oplus^2\,F(q)}.

proposition: Earth-read reconstructions on the declared Solar-System window. From reference,

κ(q)=1RF(q),Ξ(q)=1κ(q)2,\kappa_\oplus(q)=\sqrt{\frac{1}{R\,F(q)}},\qquad \Xi_\oplus(q)=1-\kappa_\oplus(q)^2,
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\kappa_\oplus(q)=\sqrt{\frac{1}{R\,F(q)}},\qquad
\Xi_\oplus(q)=1-\kappa_\oplus(q)^2,

and since dτ=κdTd\tau=\kappa_\oplus dTd\tau=\kappa_\oplus dT at rr_\oplusr_\oplus,

T0(q)=τ0κ(q).T_0(q)=\frac{\tau_0}{\kappa_\oplus(q)}.
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T_0(q)=\frac{\tau_0}{\kappa_\oplus(q)}.

Moreover, define the Earth-unit path-normalization readout by

Vreadc=1κpath=1κ(q)F(q)=RF(q).\frac{V_{\rm read}}{c_\oplus}=\frac{1}{\kappa_{\mathrm{path}}} =\frac{1}{\kappa_\oplus(q)\,F(q)}=\sqrt{\frac{R}{F(q)}}.
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\frac{V_{\rm read}}{c_\oplus}=\frac{1}{\kappa_{\mathrm{path}}}
=\frac{1}{\kappa_\oplus(q)\,F(q)}=\sqrt{\frac{R}{F(q)}}.

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05

Completion functional

Operational decision variableCompletion functional

A closure-based normalization is only as strong as the operational closure that implements it. In radiometric tracking, coherent two-way/three-way DSN links realize a phase-coherent uplink/downlink loop: the spacecraft transponder locks the downlink to the received uplink (up to a fixed turnaround ratio), and the ground receiver counts accumulated carrier phase over a declared count interval [citation]. We remove ambiguity by fixing (i) a single operational decision variable SSS and (ii) a single completion functional C\mathcal{C}\mathcal{C} that is defined as the minimal phase accumulation required to flip SSS within the same declared pipeline.

Operational decision variable

definition: Sign-distinguishing completion variable. Fix a declared phase-discriminator pipeline that outputs a real-valued discriminator signal y(t)y(t)y(t), and fix a measurement window of duration TwT_wT_w. Assume that, within the declared pipeline, y(t)y(t)y(t) is (up to a fixed gain and offset) a sinusoid of a dimensionless phase argument, e.g.\ y(t)cosθ(t)y(t)\propto \cos\theta(t)y(t)\propto \cos\theta(t) or y(t)sinθ(t)y(t)\propto \sin\theta(t)y(t)\propto \sin\theta(t). This covers an interferometric difference channel, coherent I/Q discrimination (Lemma reference), and multiplier phase detection (Lemma reference). Define the binary decision variable

Ssign ⁣(t0t0+Twy(t)dt){+1,1}.S \equiv \operatorname{sign}\!\left(\int_{t_0}^{t_0+T_w} y(t)\,dt\right)\in\{+1,-1\}.
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S \equiv \operatorname{sign}\!\left(\int_{t_0}^{t_0+T_w} y(t)\,dt\right)\in\{+1,-1\}.

A completion is an operational transformation that flips SSS while remaining within the same declared measurement pipeline.

remark: Interference/discriminator readout and the pipeline phase argument. The detector outputs used here depend sinusoidally on a phase-error coordinate; the elementary trigonometric forms are written explicitly in Lemma reference and Lemma reference. The sign decision in reference is therefore a fixed functional of a dimensionless phase-like pipeline coordinate.

In the task class used below, the phase argument is not identified with the raw carrier phase ωt\omega t\omega t. Instead, the declared DSN phase-count pipeline constructs a frequency-free coordinate from radiometric observables by pairing an observed total-count phase PobsP_{\mathrm{obs}}P_{\mathrm{obs}} with its computed reference P0P_{0}P_{0} under the minimal computed-model conditions of Definition reference and forming the ratio ΔΘ(γ)=Φ(γ)=Pobs(γ)/P0(γ)\Delta\Theta(\gamma)=\Phi(\gamma)=P_{\mathrm{obs}}(\gamma)/P_0(\gamma)\Delta\Theta(\gamma)=\Phi(\gamma)=P_{\mathrm{obs}}(\gamma)/P_0(\gamma) (Definition reference) [citation]. The admissibility gate in Definition reference prevents conjunction-dependent solar-plasma contamination from reintroducing an effective variable cutoff on the declared Solar-System window. Because Φ\Phi\Phi is a ratio of like-typed observed/computed cycle counts, the cycles-to-radians conversion cancels identically (Lemma reference), so no extra 2π2\pi2\pi factor remains at the level of ΔΘ\Delta\Theta\Delta\Theta.

The relevant closure is operational: coherent two-way/three-way DSN links realize a phase-coherent uplink/downlink loop with a fixed transponder turnaround ratio [citation]. One-way non-coherent links depend on an independent spacecraft oscillator and therefore break this closure, providing an internal control in Sec. reference. Accordingly, any nondegenerate binary detector formed within the declared coherent pipeline belongs, up to fixed gain and phase offset, to the first-harmonic family D(Θ)=sign(acosΘ+bsinΘ)D(\Theta)=\operatorname{sign}(a\cos\Theta+b\sin\Theta)D(\Theta)=\operatorname{sign}(a\cos\Theta+b\sin\Theta).

lemma: Coherent I/Q phase discriminator yields sinusoidal outputs. Consider a coherent in-phase/quadrature-phase detector for a received carrier of the form s(t)=Acm(t)cos(2πfct)s(t)=A_c m(t)\cos(2\pi f_c t)s(t)=A_c m(t)\cos(2\pi f_c t) mixed with local oscillators cos(2πfct+φ)\cos(2\pi f_c t+\varphi)\cos(2\pi f_c t+\varphi) and sin(2πfct+φ)\sin(2\pi f_c t+\varphi)\sin(2\pi f_c t+\varphi), followed by ideal low-pass filtering. Then the baseband components satisfy

vI(t)=Ac2m(t)cosφ,vQ(t)=Ac2m(t)sinφ,v_I(t)=\frac{A_c}{2}\,m(t)\cos\varphi,\qquad v_Q(t)=\frac{A_c}{2}\,m(t)\sin\varphi,
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v_I(t)=\frac{A_c}{2}\,m(t)\cos\varphi,\qquad v_Q(t)=\frac{A_c}{2}\,m(t)\sin\varphi,

up to an overall amplitude normalization. Thus coherent phase discrimination naturally produces cosφ\cos\varphi\cos\varphi and sinφ\sin\varphi\sin\varphi terms of a phase-error coordinate φ\varphi\varphi.

proof. Multiply s(t)s(t)s(t) by cos(2πfct+φ)\cos(2\pi f_c t+\varphi)\cos(2\pi f_c t+\varphi) and use cosacosb=12[cos(ab)+cos(a+b)]\cos a\cos b=\tfrac{1}{2}[\cos(a-b)+\cos(a+b)]\cos a\cos b=\tfrac{1}{2}[\cos(a-b)+\cos(a+b)]; after low-pass filtering the high-frequency term, one obtains vI(t)=(Ac/2)m(t)cosφv_I(t)=(A_c/2)m(t)\cos\varphiv_I(t)=(A_c/2)m(t)\cos\varphi. The quadrature branch follows similarly using cosasinb=12[sin(ba)+sin(b+a)]\cos a\sin b=\tfrac{1}{2}[\sin(b-a)+\sin(b+a)]\cos a\sin b=\tfrac{1}{2}[\sin(b-a)+\sin(b+a)], yielding vQ(t)=(Ac/2)m(t)sinφv_Q(t)=(A_c/2)m(t)\sin\varphiv_Q(t)=(A_c/2)m(t)\sin\varphi after low-pass filtering. This is the standard coherent I/Q low-pass reduction.

In coherent carrier tracking, these sinusoidal discriminator outputs are used to form a phase-error signal for a phase-locked loop. This is the operational setting of coherent Doppler tracking receivers, including DSN carrier tracking loops used for radiometric Doppler measurement [citation].

lemma: Multiplier phase detector output is proportional to cosφ\cos\varphi\cos\varphi. Let x(t)=Acos(ωt)x(t)=A\cos(\omega t)x(t)=A\cos(\omega t) and y(t)=Bcos(ωt+φ)y(t)=B\cos(\omega t+\varphi)y(t)=B\cos(\omega t+\varphi) be two sinusoids with phase difference φ\varphi\varphi. The low-pass filtered product satisfies

LPF{x(t)y(t)}=AB2cosφ,\mathrm{LPF}\{x(t)y(t)\}=\frac{AB}{2}\cos\varphi,
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\mathrm{LPF}\{x(t)y(t)\}=\frac{AB}{2}\cos\varphi,

up to a fixed gain, so a multiplier phase detector naturally produces a cos(phase error)\cos(\text{phase error})\cos(\text{phase error}) output.

proof. Using cosacosb=12[cos(ab)+cos(a+b)]\cos a\cos b=\tfrac{1}{2}[\cos(a-b)+\cos(a+b)]\cos a\cos b=\tfrac{1}{2}[\cos(a-b)+\cos(a+b)] gives

x(t)y(t)=AB2cosφ+AB2cos(2ωt+φ).x(t)y(t)=\frac{AB}{2}\cos\varphi+\frac{AB}{2}\cos(2\omega t+\varphi).
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x(t)y(t)=\frac{AB}{2}\cos\varphi+\frac{AB}{2}\cos(2\omega t+\varphi).

Low-pass filtering removes the 2ω2\omega2\omega term, leaving reference.

lemma: First-harmonic detector universality forces the antipodal completion. After centering each coherent detector to zero threshold and absorbing fixed gains and phase offsets into the coefficients, every nondegenerate binary detector produced within the declared coherent pipeline has the form

D(Θ)=sign ⁣(acosΘ+bsinΘ),(a,b)(0,0).D(\Theta)=\operatorname{sign}\!\big(a\cos\Theta+b\sin\Theta\big),\qquad (a,b)\neq(0,0).
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D(\Theta)=\operatorname{sign}\!\big(a\cos\Theta+b\sin\Theta\big),\qquad (a,b)\neq(0,0).

Equivalently,

D(Θ)=sign ⁣(Rcos(Θϕ)),R>0.D(\Theta)=\operatorname{sign}\!\big(R\cos(\Theta-\phi)\big),\qquad R>0.
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D(\Theta)=\operatorname{sign}\!\big(R\cos(\Theta-\phi)\big),\qquad R>0.

Its zero set is an antipodal pair on S1S^1S^1, and the unique minimal global phase shift that flips the decision on every coherent phase class is

ΔΘ=π.|\Delta\Theta|=\pi.
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|\Delta\Theta|=\pi.

Thus the sign-distinguishing completion task is universal across the centered coherent first-harmonic detector family realized by the declared pipeline.

proof. By Lemma reference, coherent I/Q discrimination produces outputs proportional to cosΘ\cos\Theta\cos\Theta and sinΘ\sin\Theta\sin\Theta. By Lemma reference, multiplier phase detection produces the same first-harmonic family. After centering to zero threshold and absorbing fixed gains and phase offsets into the coefficients, any nondegenerate binary detector formed from these coherent outputs has the form

D(Θ)=sign ⁣(acosΘ+bsinΘ)=sign ⁣(Rcos(Θϕ)).D(\Theta)=\operatorname{sign}\!\big(a\cos\Theta+b\sin\Theta\big) =\operatorname{sign}\!\big(R\cos(\Theta-\phi)\big).
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D(\Theta)=\operatorname{sign}\!\big(a\cos\Theta+b\sin\Theta\big)
=\operatorname{sign}\!\big(R\cos(\Theta-\phi)\big).

The zero set of Rcos(Θϕ)R\cos(\Theta-\phi)R\cos(\Theta-\phi) consists of the antipodal pair Θ=ϕ±π/2\Theta=\phi\pm \pi/2\Theta=\phi\pm \pi/2. Hence the positive and negative decision classes are complementary open semicircles. Any global phase shift of magnitude strictly less than π\pi\pi leaves a nonempty arc within the same sign class and therefore cannot flip the detector on every coherent phase class. The shift ΘΘ+π\Theta\mapsto \Theta+\pi\Theta\mapsto \Theta+\pi maps each semicircle to its complement and flips the sign everywhere. Therefore the unique minimal global completion for the full coherent first-harmonic detector family is ΔΘ=π|\Delta\Theta|=\pi|\Delta\Theta|=\pi.

lemma: Cycles-to-radians conversion cancels in the phase ratio. Let Ψobs(γ)2πPobs(γ)\Psi_{\mathrm{obs}}(\gamma)\equiv 2\pi P_{\mathrm{obs}}(\gamma)\Psi_{\mathrm{obs}}(\gamma)\equiv 2\pi P_{\mathrm{obs}}(\gamma) and Ψ0(γ)2πP0(γ)\Psi_{0}(\gamma)\equiv 2\pi P_{0}(\gamma)\Psi_{0}(\gamma)\equiv 2\pi P_{0}(\gamma) denote the corresponding accumulated phases in radians. Then

Ψobs(γ)Ψ0(γ)=Pobs(γ)P0(γ)=Φ(γ).\frac{\Psi_{\mathrm{obs}}(\gamma)}{\Psi_{0}(\gamma)}=\frac{P_{\mathrm{obs}}(\gamma)}{P_{0}(\gamma)}=\Phi(\gamma).
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\frac{\Psi_{\mathrm{obs}}(\gamma)}{\Psi_{0}(\gamma)}=\frac{P_{\mathrm{obs}}(\gamma)}{P_{0}(\gamma)}=\Phi(\gamma).

In particular, the conventional cycles-to-radians factor 2π2\pi2\pi cancels identically in the ratio used to define Φ\Phi\Phi.

proof. This is immediate from the definitions Ψobs=2πPobs\Psi_{\mathrm{obs}}=2\pi P_{\mathrm{obs}}\Psi_{\mathrm{obs}}=2\pi P_{\mathrm{obs}} and Ψ0=2πP0\Psi_{0}=2\pi P_{0}\Psi_{0}=2\pi P_{0}.

lemma: No multiplicative ambiguity in the pipeline phase scale. Under Definition reference, the pipeline phase coordinate is fixed as the normalized phase-count ratio ΔΘ(γ)=Φ(γ)=Pobs(γ)/P0(γ)\Delta\Theta(\gamma)=\Phi(\gamma)=P_{\mathrm{obs}}(\gamma)/P_{0}(\gamma)\Delta\Theta(\gamma)=\Phi(\gamma)=P_{\mathrm{obs}}(\gamma)/P_{0}(\gamma). In particular, for a constant-κ\kappa\kappa segment γ\gamma\gamma with κ()κ0\kappa(\ell)\equiv \kappa_0\kappa(\ell)\equiv \kappa_0, the ratio satisfies ΔΘ(γ)=tprop(γ)/t0(γ)=1/κ0\Delta\Theta(\gamma)=t_{\mathrm{prop}}(\gamma)/t_{0}(\gamma)=1/\kappa_0\Delta\Theta(\gamma)=t_{\mathrm{prop}}(\gamma)/t_{0}(\gamma)=1/\kappa_0. Therefore any rescaling ΔΘkΔΘ\Delta\Theta\mapsto k\,\Delta\Theta\Delta\Theta\mapsto k\,\Delta\Theta with k1k\neq 1k\neq 1 would contradict the defining normalization and correspond to a different declared pipeline. The model thus contains no undetermined multiplicative factor in the discriminator phase argument.

proof. If κ()κ0\kappa(\ell)\equiv \kappa_0\kappa(\ell)\equiv \kappa_0 on γ\gamma\gamma, then by reference we have v()=Vκ0v(\ell)=V\kappa_0v(\ell)=V\kappa_0 and hence

tprop(γ)=γdVκ0=LγVκ0,t0(γ)=LγV.t_{\mathrm{prop}}(\gamma)=\int_\gamma \frac{d\ell}{V\kappa_0}=\frac{L_\gamma}{V\kappa_0},\qquad t_{0}(\gamma)=\frac{L_\gamma}{V}.
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t_{\mathrm{prop}}(\gamma)=\int_\gamma \frac{d\ell}{V\kappa_0}=\frac{L_\gamma}{V\kappa_0},\qquad
t_{0}(\gamma)=\frac{L_\gamma}{V}.

Thus ΔΘ(γ)=tprop(γ)/t0(γ)=1/κ0\Delta\Theta(\gamma)=t_{\mathrm{prop}}(\gamma)/t_{0}(\gamma)=1/\kappa_0\Delta\Theta(\gamma)=t_{\mathrm{prop}}(\gamma)/t_{0}(\gamma)=1/\kappa_0. Since Definition reference identifies ΔΘ\Delta\Theta\Delta\Theta with this measured ratio, multiplying it by a constant k1k\neq 1k\neq 1 breaks the defining normalization.

proposition: Gauge-fixed phase-error coordinate. Let a declared DSN phase-count pipeline produce the ratio Φ(γ)=Pobs(γ)/P0(γ)\Phi(\gamma)=P_{\mathrm{obs}}(\gamma)/P_{0}(\gamma)\Phi(\gamma)=P_{\mathrm{obs}}(\gamma)/P_{0}(\gamma) (Definition reference). Consider any alternative discriminator coordinate of the form Θ~(γ)=g(Φ(γ))\tilde{\Theta}(\gamma)=g(\Phi(\gamma))\tilde{\Theta}(\gamma)=g(\Phi(\gamma)) used in place of ΔΘ(γ)=Φ(γ)\Delta\Theta(\gamma)=\Phi(\gamma)\Delta\Theta(\gamma)=\Phi(\gamma). If Θ~\tilde{\Theta}\tilde{\Theta} satisfies the constant-κ\kappa\kappa normalization g(1/κ0)=1/κ0g(1/\kappa_0)=1/\kappa_0g(1/\kappa_0)=1/\kappa_0 for all κ0(0,1]\kappa_0\in(0,1]\kappa_0\in(0,1] (Lemma reference), then ggg is the identity on the admissible domain and Θ~(γ)=Φ(γ)\tilde{\Theta}(\gamma)=\Phi(\gamma)\tilde{\Theta}(\gamma)=\Phi(\gamma).

proof. For any κ0(0,1]\kappa_0\in(0,1]\kappa_0\in(0,1], the constant-κ\kappa\kappa case gives Φ=1/κ0[1,)\Phi=1/\kappa_0\in[1,\infty)\Phi=1/\kappa_0\in[1,\infty) and requires g(Φ)=Φg(\Phi)=\Phig(\Phi)=\Phi. Thus g(x)=xg(x)=xg(x)=x for all x[1,)x\in[1,\infty)x\in[1,\infty), which is the admissible range of Φ\Phi\Phi under κ(0,1]\kappa\in(0,1]\kappa\in(0,1]. Therefore Θ~(γ)=Φ(γ)\tilde{\Theta}(\gamma)=\Phi(\gamma)\tilde{\Theta}(\gamma)=\Phi(\gamma) and the discriminator phase-error coordinate is gauge-fixed by the declared DSN pipeline.

theorem: Maximal invariant of DSN phase-count data. Fix a declared DSN phase-count pipeline satisfying the minimal computed model contract (Definition reference) and the admissibility gate (Definition reference), so that (Pobs,P0)R>02(P_{\mathrm{obs}},P_0)\in\mathbb{R}_{>0}^2(P_{\mathrm{obs}},P_0)\in\mathbb{R}_{>0}^2 denotes an observed/computed total-count phase pair (cycles) for the same DSN data type and count interval. Consider the group of positive scalings

ga: (Pobs,P0)(aPobs,aP0),a>0,g_a:\ (P_{\mathrm{obs}},P_0)\mapsto (aP_{\mathrm{obs}},aP_0),\qquad a>0,
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g_a:\ (P_{\mathrm{obs}},P_0)\mapsto (aP_{\mathrm{obs}},aP_0),\qquad a>0,

which captures carrier-frequency scaling and unit conversions (including cycles-to-radians). Then the ratio

Φ=PobsP0\Phi=\frac{P_{\mathrm{obs}}}{P_0}
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\Phi=\frac{P_{\mathrm{obs}}}{P_0}

is a maximal invariant: any statistic invariant under gag_ag_a is a function of Φ\Phi\Phi [citation].

proof. If (Pobs,P0)=ga(Pobs,P0)(P_{\mathrm{obs}}',P_0')=g_a(P_{\mathrm{obs}},P_0)(P_{\mathrm{obs}}',P_0')=g_a(P_{\mathrm{obs}},P_0) then Pobs/P0=Pobs/P0P_{\mathrm{obs}}'/P_0'=P_{\mathrm{obs}}/P_0P_{\mathrm{obs}}'/P_0'=P_{\mathrm{obs}}/P_0. Conversely, if Pobs/P0=Pobs/P0P_{\mathrm{obs}}'/P_0'=P_{\mathrm{obs}}/P_0P_{\mathrm{obs}}'/P_0'=P_{\mathrm{obs}}/P_0, then choosing a=P0/P0a=P_0'/P_0a=P_0'/P_0 yields (aPobs,aP0)=(Pobs,P0)(aP_{\mathrm{obs}},aP_0)=(P_{\mathrm{obs}}',P_0')(aP_{\mathrm{obs}},aP_0)=(P_{\mathrm{obs}}',P_0'). Hence the orbits of the scaling group are indexed by Φ\Phi\Phi, making it maximal invariant. Any invariant statistic must be constant on orbits and therefore is a function of Φ\Phi\Phi.

remark: Invariant procedures depend only on Φ\Phi\Phi. By Theorem reference, Φ\Phi\Phi is a maximal invariant under the phase-count scaling group for any declared DSN phase-count pipeline satisfying Definition reference and Definition reference, hence any invariant statistic---and therefore any invariant estimation or testing procedure for curvature layering within the declared DSN/PLL pipeline---is necessarily a function of Φ\Phi\Phi [citation]. Together with the constant-κ\kappa\kappa gauge fixing in Proposition reference, this closes the invariant phase-error coordinate choice without invoking an explicit noise model.

Completion functional Let ΔΘ(γ)\Delta\Theta(\gamma)\Delta\Theta(\gamma) denote the frequency-free phase-like shift produced by the fixed pipeline for a path γ\gamma\gamma in a domain D\mathcal{D}\mathcal{D}. We define it by the dimensionless layered path functional in Definition reference:

ΔΘ(γ)Φ(γ)=1Lγγdκ().\Delta\Theta(\gamma)\equiv \Phi(\gamma)=\frac{1}{L_\gamma}\int_{\gamma}\frac{d\ell}{\kappa(\ell)}.
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\Delta\Theta(\gamma)\equiv \Phi(\gamma)=\frac{1}{L_\gamma}\int_{\gamma}\frac{d\ell}{\kappa(\ell)}.

definition: Task-fixed completion functional. Let Γ\Gamma\Gamma be a declared class of admissible paths in D\mathcal{D}\mathcal{D}. Define the completion functional as

C[Γ;D]infγΓ{ΔΘ(γ): S flips under the induced phase shift}.\mathcal{C}[\Gamma;\mathcal{D}] \equiv \inf_{\gamma\in\Gamma}\{|\Delta\Theta(\gamma)|:\ S \text{ flips under the induced phase shift}\}.
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\mathcal{C}[\Gamma;\mathcal{D}] \equiv
\inf_{\gamma\in\Gamma}\{|\Delta\Theta(\gamma)|:\ S \text{ flips under the induced phase shift}\}.

The functional ΔΘ\Delta\Theta\Delta\Theta in reference is the measured phase-like output of the fixed pipeline (not a free mathematical surrogate) and is frequency-free by construction. The quantity C\mathcal{C}\mathcal{C} is therefore a task-bound lower bound over the declared class Γ\Gamma\Gamma; equality between C\mathcal{C}\mathcal{C} and a realized path value is not automatic. Such an equality is used only after the normalization class has been fixed and the representative readout has been shown to be class-bound on the declared normalization class, as in Lemma reference.

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06

Normalization witnesses for the task-fixed completionNormalization witnesses for the task-fixed completion

Witness A: antipodal sign flip and bounded half-waveWitness B: half-geodesic ring representative

The following lemmas do not supply independent Solar-System reconstruction theorems. They identify reference representatives inside the declared completion family that compute the same task-fixed functional C\mathcal{C}\mathcal{C} and therefore serve only as normalization witnesses.

Witness A: antipodal sign flip and bounded half-wave

lemma: Half-turn \leftrightarrow\leftrightarrow half-wave. In the sign-distinguishing completion task reference, the minimal phase accumulation that flips SSS is π\pi\pi. A bounded interval representative reads the same task as the fundamental half-wave condition kL=πkL=\pikL=\pi.

proof. By the convention fixed in Remark reference, the discriminator is applied to the pipeline phase ΔΘ(t)\Delta\Theta(t)\Delta\Theta(t), so y(t)y(t)y(t) is (up to a fixed gain/offset) a sinusoid of ΔΘ(t)\Delta\Theta(t)\Delta\Theta(t), e.g.\ y(t)cos(ΔΘ(t))y(t)\propto \cos(\Delta\Theta(t))y(t)\propto \cos(\Delta\Theta(t)) (or sin\sin\sin under a fixed phase offset). A sign flip of the integrated signal in reference occurs under a phase inversion ΔΘΔΘ+π\Delta\Theta\mapsto \Delta\Theta+\pi\Delta\Theta\mapsto \Delta\Theta+\pi because cos(ΔΘ+π)=cos(ΔΘ)\cos(\Delta\Theta+\pi)=-\cos(\Delta\Theta)\cos(\Delta\Theta+\pi)=-\cos(\Delta\Theta) (and similarly for sin\sin\sin). Hence any completion that flips SSS must satisfy ΔΘπ|\Delta\Theta|\ge \pi|\Delta\Theta|\ge \pi, and the bound is achieved by the half-turn shift ΔΘ=π|\Delta\Theta|=\pi|\Delta\Theta|=\pi.

For the bounded-mode representation, take a standing-wave representative ψ(x)=Asin(kx)\psi(x)=A\sin(kx)\psi(x)=A\sin(kx) on x[0,L]x\in[0,L]x\in[0,L] with nodes (fixed endpoints) ψ(0)=ψ(L)=0\psi(0)=\psi(L)=0\psi(0)=\psi(L)=0. Separation of variables with these boundary conditions yields the fundamental mode kL=πkL=\pikL=\pi. This half-wave condition yields the same minimal sign-distinguishing closure constant π\pi\pi.

Witness B: half-geodesic ring representative

lemma: Half-wave \leftrightarrow\leftrightarrow half-geodesic on a ring. Consider a ring domain of radius RRR with arclength coordinate sss and a phase accumulation ΔΘ=k\Delta\Theta = k\ell\Delta\Theta = k\ell along a path of length \ell\ell. Within the declared completion family, a ring representative reads the minimal sign-distinguishing completion as a half-geodesic length =πR\ell=\pi R\ell=\pi R and therefore carries the same π\pi\pi normalization.

proof. On a ring, the half-geodesic between antipodal points has arclength =πR\ell=\pi R\ell=\pi R. Under a phase-gradient description with constant effective wavenumber kkk along the path, the phase accumulation is ΔΘ=k\Delta\Theta=k\ell\Delta\Theta=k\ell. By Lemma reference, the minimal sign-distinguishing completion requires ΔΘ=π|\Delta\Theta|=\pi|\Delta\Theta|=\pi. Hence the fundamental completion scale on the ring satisfies k(πR)=πk(\pi R)=\pik(\pi R)=\pi, which is the same π\pi\pi normalization as the half-wave closure kL=πkL=\pikL=\pi with L=πRL=\pi RL=\pi R.

remark: Geometric scope. The ring is used only as a reference representative inside the declared completion family. No appeal to spherical great-circle geometry is required, and no independent Solar-System reconstruction claim is made at this step.

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07

Task-fixed normalizationTask-fixed normalization

Task-fixed completion constantNormalization and uniqueness of a frequency-free completion/ propagation functional

remark: Implication status of the calibration theorem chain. The theorem chain in this section is implication-relative. The admissibility of the Solar-System window, the delay-channel reconstruction principle, the Herglotz monotonicity condition, the angular/lens witness package, and the boundary normalization are treated as declared hypotheses of Contract C\mathsf C\mathsf C. The implication content used for the final readout is the consequence chain from those hypotheses to the class-bound readouts

C=π,Vread/c=π,R=π2F(3/4),D0=τ0π2F(3/4).\mathcal C=\pi, \qquad V_{\rm read}/c_\oplus=\pi, \qquad R=\pi^2F(3/4), \qquad D_0=\tau_0\pi^2F(3/4).
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\mathcal C=\pi,
\qquad
V_{\rm read}/c_\oplus=\pi,
\qquad
R=\pi^2F(3/4),
\qquad
D_0=\tau_0\pi^2F(3/4).

Thus the claim is not a new general proof of lens rigidity, not a universal propagation law, and not a cosmological horizon theorem. It is a declared-class implication under the stated calibration package.

Task-fixed completion constant

theorem: Declared-task completion constant on the coherent first-harmonic detector family. For the completion task defined by reference--reference, the task-bound completion functional satisfies

C=π.\mathcal{C}=\pi.
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\mathcal{C}=\pi.

This theorem fixes only the completion constant of the declared coherent first-harmonic task. It is a task-fixed completion statement, not a universal geometrical theorem for π\pi\pi, not a general propagation theorem, and not an empirical horizon measurement. It does not by itself select a Solar-System κ\kappa\kappa-profile, does not by itself select the normalization class Γπ\Gamma_\pi\Gamma_\pi, and does not by itself imply Vread/c=πV_{\rm read}/c_\oplus=\piV_{\rm read}/c_\oplus=\pi. If the range/Doppler observables, the task-boundary conditions, or the witness package needed to select Γπ\Gamma_\pi\Gamma_\pi fail, the declared class-bound readout is rejected rather than reinterpreted.

proof. By Lemma reference, every nondegenerate binary detector in the coherent first-harmonic detector family has the same minimal completion threshold ΔΘ=π|\Delta\Theta|=\pi|\Delta\Theta|=\pi for the declared sign-distinguishing task. Lemma reference reads this threshold on a bounded interval representative, and Lemma reference reads the same threshold on a half-geodesic ring representative. By Proposition reference and Theorem reference, the task is evaluated on the gauge-fixed invariant coordinate ΔΘ\Delta\Theta\Delta\Theta, so carrier-frequency scaling, unit rescalings, and detector-dependent first-harmonic reparameterizations cannot change the task-fixed constant. These steps prove only the task-fixed value C=π\mathcal C=\pi\mathcal C=\pi; the later Earth-unit path-normalization ratio requires the separate normalization-class selection of Lemma reference.

Normalization and uniqueness of a frequency-free completion/ propagation functional

lemma: Constant-κ\kappa\kappa normalization is forced. If κ()κ0\kappa(\ell)\equiv \kappa_0\kappa(\ell)\equiv \kappa_0 is constant along a propagation segment γ\gamma\gamma, then the phase-ratio functional in Definition reference satisfies

Φ(γ)=1κ0.\Phi(\gamma)=\frac{1}{\kappa_0}.
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\Phi(\gamma)=\frac{1}{\kappa_0}.

proof. If κ()κ0\kappa(\ell)\equiv \kappa_0\kappa(\ell)\equiv \kappa_0, then v()=Vκ0v(\ell)=V\kappa_0v(\ell)=V\kappa_0 by reference. Therefore

tprop(γ)=γdVκ0=LγVκ0.t_{\mathrm{prop}}(\gamma)=\int_{\gamma}\frac{d\ell}{V\kappa_0}=\frac{L_\gamma}{V\kappa_0}.
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t_{\mathrm{prop}}(\gamma)=\int_{\gamma}\frac{d\ell}{V\kappa_0}=\frac{L_\gamma}{V\kappa_0}.

Dividing by Lγ/VL_\gamma/VL_\gamma/V gives Φ(γ)=tprop(γ)/(Lγ/V)=1/κ0\Phi(\gamma)=t_{\mathrm{prop}}(\gamma)/(L_\gamma/V)=1/\kappa_0\Phi(\gamma)=t_{\mathrm{prop}}(\gamma)/(L_\gamma/V)=1/\kappa_0.

theorem: Representation theorem for the frequency-free phase-ratio functional. Let γ\gamma\gamma be a propagation segment of Euclidean length LγγdL_\gamma\equiv\int_\gamma d\ellL_\gamma\equiv\int_\gamma d\ell with piecewise-continuous κ()(0,1]\kappa(\ell)\in(0,1]\kappa(\ell)\in(0,1]. Consider a frequency-free, dimensionless pipeline variable ΔΘ(γ)\Delta\Theta(\gamma)\Delta\Theta(\gamma) that satisfies: (i) on constant-κ\kappa\kappa segments, ΔΘ(γ)=Φ(γ)\Delta\Theta(\gamma)=\Phi(\gamma)\Delta\Theta(\gamma)=\Phi(\gamma) (equivalently reference); and (ii) for piecewise-constant approximations of κ()\kappa(\ell)\kappa(\ell), ΔΘ(γ)\Delta\Theta(\gamma)\Delta\Theta(\gamma) is refinement-stable and depends only on the segment lengths and constant values (Riemann-sum consistency). Then necessarily

ΔΘ(γ)=1Lγγdκ(),\Delta\Theta(\gamma)=\frac{1}{L_\gamma}\int_{\gamma}\frac{d\ell}{\kappa(\ell)},
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\Delta\Theta(\gamma)=\frac{1}{L_\gamma}\int_{\gamma}\frac{d\ell}{\kappa(\ell)},

and this choice is unique under (i)--(ii).

proof. Approximate κ()\kappa(\ell)\kappa(\ell) by a piecewise-constant profile {κi}\{\kappa_i\}\{\kappa_i\} on segments of lengths {i}\{\ell_i\}\{\ell_i\} with ii=Lγ\sum_i \ell_i=L_\gamma\sum_i \ell_i=L_\gamma. By (i), on each constant segment the pipeline variable must reduce to 1/κi1/\kappa_i1/\kappa_i. Refinement stability (ii) then forces the normalized Riemann-sum form

ΔΘ(γ)=1Lγiiκi,\Delta\Theta(\gamma)=\frac{1}{L_\gamma}\sum_i \frac{\ell_i}{\kappa_i},
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\Delta\Theta(\gamma)=\frac{1}{L_\gamma}\sum_i \frac{\ell_i}{\kappa_i},

which converges to reference in the continuum limit. Uniqueness follows because any alternative refinement-stable construction with the same constant-κ\kappa\kappa normalization must agree on all piecewise-constant profiles and hence on their limit.

remark: Tracking observables and refinement stability. In the DSN, a Doppler measurement consists of accumulated carrier phase measurements, from which frequency is obtained as the rate-of-change of phase; the measurement is reported over a declared count interval and depends on the one-way/two-way/three-way link definition [citation]. The DSN Services Catalog summarizes the accuracy and count-time behavior of Doppler tracking and its dependence on observing conditions [citation]. In navigation processing, these observed phase-count or Doppler data are paired with computed values for the same DSN data type and count interval under a declared model [citation]. This operational ``accumulate over sub-intervals and compare to computed'' structure motivates the refinement stability (ii) used above.

lemma: Earth-unit path-normalization ratio on the declared Solar-System reference path. For the Solar-System reference path in reference,

Vreadc=κpath1=Φ,\frac{V_{\rm read}}{c_\oplus}=\kappa_{\mathrm{path}}^{-1}=\Phi,
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\frac{V_{\rm read}}{c_\oplus}=\kappa_{\mathrm{path}}^{-1}=\Phi,

where Φ\Phi\Phi is the dimensionless layered path functional in Definition reference, and VreadV_{\rm read}V_{\rm read} denotes only the exported normalized path-readout variable on the declared calibration class.

proof. From reference, the dimensionless Earth-unit path-normalization readout on the reference segment is

Vreadc=1Lrrdrκ(r).\frac{V_{\rm read}}{c_\oplus}=\frac{1}{L}\int_{r_\odot}^{r_\oplus}\frac{dr}{\kappa(r)}.
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\frac{V_{\rm read}}{c_\oplus}=\frac{1}{L}\int_{r_\odot}^{r_\oplus}\frac{dr}{\kappa(r)}.

Therefore Vread/c=(1/L)rrdr/κ(r)=ΦV_{\rm read}/c_\oplus=(1/L)\int_{r_\odot}^{r_\oplus}dr/\kappa(r)=\PhiV_{\rm read}/c_\oplus=(1/L)\int_{r_\odot}^{r_\oplus}dr/\kappa(r)=\Phi by Definition reference.

lemma: Boundary-normalized selection of the declared normalization class within the radial-isotropic class. For the Earth-unit path-normalization readout defined in reference, use the joint boundary-normalized package consisting of (a) the travel-time functional Φ\Phi\Phi and (b) an admissible angular/lens witness for the same Solar-System window. Assume (i) central isotropy, (ii) admissible solar-window convexity in Definition reference, and (iii) within the declared radial-isotropic class, any competing profile with the same boundary normalization and the same delay data must also reproduce the same admissible angular/lens data. Then, within the declared class, the admissible candidates are accepted as a single boundary-normalized radial equivalence class up to boundary-fixing gauge. Consequently the declared π\pi\pi-normalization class used for the class-bound path-normalization readout may be taken to be the selected boundary-normalized radial reparameterization class Γπ\Gamma_\pi\Gamma_\pi of the segment from rr_\odotr_\odot to rr_\oplusr_\oplus; if γref\gamma_{\mathrm{ref}}\gamma_{\mathrm{ref}} denotes its reference representative, then ΔΘ\Delta\Theta\Delta\Theta is constant on Γπ\Gamma_\pi\Gamma_\pi and

C[Γπ;D]=ΔΘ(γref).\mathcal{C}[\Gamma_\pi;\mathcal{D}] = \left|\Delta\Theta(\gamma_{\mathrm{ref}})\right|.
TeX source
\mathcal{C}[\Gamma_\pi;\mathcal{D}]
=
\left|\Delta\Theta(\gamma_{\mathrm{ref}})\right|.

proof. The role of the angular channel here is not to reprove a new general rigidity theorem from scratch. Rather, within the declared radial-isotropic class, the classical Herglotz--Abel inversion and modern boundary/lens-rigidity results provide the admissibility support used here: for radial isotropic profiles satisfying reference, travel-time data determine the radial refractive profile n(r)1/κ(r)n(r)\propto 1/\kappa(r)n(r)\propto 1/\kappa(r), while lens data under the same boundary normalization remove competing profiles up to the natural boundary-fixing gauge under the usual convexity hypotheses [citation]. The angular witness contemplated here is operationally available through Delta-DOR/VLBI-type sky-plane observables used alongside range and Doppler in deep-space navigation [citation]. Thus, within the declared class, admissible delay-consistent candidates that survive the angular witness are accepted as one boundary-normalized radial equivalence class.

Once that class is fixed, reference fixes the normalization problem by fixing the endpoints r,rr_\odot,r_\oplusr_\odot,r_\oplus and the reference Euclidean length L=rrL=r_\oplus-r_\odotL=r_\oplus-r_\odot for the Earth-unit path-normalization readout. The admissible representative is thus the radial segment joining the declared boundaries, unique up to orientation-preserving reparameterization. Finally, by reference, ΔΘ(γ)=Lγ1γd/κ()\Delta\Theta(\gamma)=L_\gamma^{-1}\int_\gamma d\ell/\kappa(\ell)\Delta\Theta(\gamma)=L_\gamma^{-1}\int_\gamma d\ell/\kappa(\ell) depends only on the geometric segment and is invariant under reparameterization. Hence ΔΘ\Delta\Theta\Delta\Theta is constant on Γπ\Gamma_\pi\Gamma_\pi, yielding reference.

remark: Scope of Lemma reference. The lemma is a class-selection statement within the declared radial-isotropic class. It does not amount to a fully general reproof of lens rigidity for arbitrary media or arbitrary path classes.

remark: Same-propagation-geometry reading of the angular witness. Geodetic VLBI reduction admits an equivalent formulation in which the gravitational delay is rewritten through terms explicitly linked to the light-deflection angle [citation]. This supports treating admissible angular data as an independent readout of the same light-propagation geometry rather than as a wholly unrelated second primitive, while still leaving the present analysis below the level of a full general lens-rigidity proof.

remark: Bridge from completion to the declared path-normalization readout. Four statements are logically distinct. First, Theorem reference fixes C=π\mathcal{C}=\pi\mathcal{C}=\pi as a task-bound completion constant for the coherent first-harmonic detector family. Second, Theorem reference and Lemma reference identify the declared Earth-unit path-normalization readout with the frequency-free path functional, denoted here by Vread/c=ΦV_{\rm read}/c_\oplus=\PhiV_{\rm read}/c_\oplus=\Phi. The symbol VreadV_{\rm read}V_{\rm read} is only the name of this normalized path readout; it is not a local velocity, group velocity, signal velocity, or universal propagation speed. Third, Lemma reference selects the declared boundary-normalized class Γπ\Gamma_\pi\Gamma_\pi on which the task readout is evaluated by a reference representative. Only after these three statements are combined does the class-bound equality Vread/c=πV_{\rm read}/c_\oplus=\piV_{\rm read}/c_\oplus=\pi follow. The equality is therefore a normalization readout on Γπ\Gamma_\pi\Gamma_\pi, not a universal claim that every admissible realized path attains the completion infimum.

corollary: Conditional path-normalization readout on the accepted π\pi\pi-normalization class. Assume Contract C\mathsf{C}\mathsf{C}, the accepted boundary-normalized witness package of Lemma reference, and the reference representative γrefΓπ\gamma_{\mathrm{ref}}\in\Gamma_\pi\gamma_{\mathrm{ref}}\in\Gamma_\pi used for the Earth-unit path readout in reference. Only under those assumptions,

Vreadc=π.\frac{V_{\rm read}}{c_\oplus}=\pi.
TeX source
\frac{V_{\rm read}}{c_\oplus}=\pi.

This is a class-bound path-normalization readout on the accepted normalization class, not a statement about arbitrary admissible paths, not a neutrino/light velocity law, and not an independent measurement of a universal propagation speed.

proof. Theorem reference gives C=π\mathcal{C}=\pi\mathcal{C}=\pi for the declared completion task only. Lemma reference supplies the additional step: on the accepted boundary-normalized class Γπ\Gamma_\pi\Gamma_\pi, the task readout is computed by the reference representative γref\gamma_{\mathrm{ref}}\gamma_{\mathrm{ref}} and therefore

C[Γπ;D]=ΔΘ(γref).\mathcal{C}[\Gamma_\pi;\mathcal{D}] = \left|\Delta\Theta(\gamma_{\mathrm{ref}})\right|.
TeX source
\mathcal{C}[\Gamma_\pi;\mathcal{D}]
=
\left|\Delta\Theta(\gamma_{\mathrm{ref}})\right|.

By Theorem reference, ΔΘ(γref)=Φ(γref)\Delta\Theta(\gamma_{\mathrm{ref}})=\Phi(\gamma_{\mathrm{ref}})\Delta\Theta(\gamma_{\mathrm{ref}})=\Phi(\gamma_{\mathrm{ref}}), and Lemma reference identifies that same representative readout with the Earth-unit path-normalization ratio,

Φ(γref)=Vreadc.\Phi(\gamma_{\mathrm{ref}})=\frac{V_{\rm read}}{c_\oplus}.
TeX source
\Phi(\gamma_{\mathrm{ref}})=\frac{V_{\rm read}}{c_\oplus}.

Combining these separate steps yields Vread/c=πV_{\rm read}/c_\oplus=\piV_{\rm read}/c_\oplus=\pi on the accepted class Γπ\Gamma_\pi\Gamma_\pi. Here VreadV_{\rm read}V_{\rm read} is the normalized path-readout variable defined in the preceding remark, not a physical velocity. If the witness package fails to select Γπ\Gamma_\pi\Gamma_\pi, the equality is not assigned.

remark: Normalization is downstream of witness acceptance. The class Γπ\Gamma_\pi\Gamma_\pi is selected only after the delay-consistent profile has survived the admissible angular witness under the same boundary normalization. The π\pi\pi readout is therefore downstream of an accepted κ\kappa\kappa-profile and is not an independent substitute for the witness package.

remark: Interpretation boundary of the readout. Corollary reference is not asserted for arbitrary admissible paths and does not claim that every realized path saturates the completion infimum. It is a class-bound readout on the declared normalization class fixed by reference and characterized in Lemma reference. Other tasks, other pipelines, or other path classes may admit different completion constants and lie outside the scope of the present claim.

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08

Declared-class Earth-unit calibration consequence under \(q=3/4\) and task-fixed completionDeclared-class Earth-unit calibration consequence under q=3/4 and task-fixed completion

Numerical evaluationContext: standard comoving scales and interpretation boundary

definition: Algebraic calibration readout package. For the final algebraic readout, the accepted calibration package exports the following equalities on the declared class:

q=34,Vreadc=π,R=F(q)(Vreadc)2,D0=τ0R.q=\frac34, \qquad \frac{V_{\rm read}}{c_\oplus}=\pi, \qquad R=F(q)\left(\frac{V_{\rm read}}{c_\oplus}\right)^2, \qquad D_0=\tau_0R.
TeX source
q=\frac34,
\qquad
\frac{V_{\rm read}}{c_\oplus}=\pi,
\qquad
R=F(q)\left(\frac{V_{\rm read}}{c_\oplus}\right)^2,
\qquad
D_0=\tau_0R.

These equalities are the consequence inputs exported by the preceding admissibility and normalization arguments. They do not by themselves assert that the accepted class exists outside the declared Solar-System calibration window.

lemma: Algebraic closure of the declared calibration readout package. Under the algebraic calibration readout package of reference,

R=π2F(3/4)andD0=τ0π2F(3/4).R=\pi^2F(3/4) \qquad\text{and}\qquad D_0=\tau_0\pi^2F(3/4).
TeX source
R=\pi^2F(3/4)
\qquad\text{and}\qquad
D_0=\tau_0\pi^2F(3/4).

proof. Substitute q=3/4q=3/4q=3/4 and Vread/c=πV_{\rm read}/c_\oplus=\piV_{\rm read}/c_\oplus=\pi into R=F(q)(Vread/c)2R=F(q)(V_{\rm read}/c_\oplus)^2R=F(q)(V_{\rm read}/c_\oplus)^2. This gives R=π2F(3/4)R=\pi^2F(3/4)R=\pi^2F(3/4). Substituting this into D0=τ0RD_0=\tau_0RD_0=\tau_0R gives D0=τ0π2F(3/4)D_0=\tau_0\pi^2F(3/4)D_0=\tau_0\pi^2F(3/4).

The final calibration is a conjunctive declared-class consequence. Six declared ingredients are used in order: additive travel time fixes the harmonic path functional (Lemma reference); the scale-free shell-extensivity premise fixes q=3/4q=3/4q=3/4 on the declared window (Proposition reference); the coherent first-harmonic completion task fixes C=π\mathcal C=\pi\mathcal C=\pi (Theorem reference); the accepted boundary-normalized class reads that completion as Vread/c=πV_{\rm read}/c_\oplus=\piV_{\rm read}/c_\oplus=\pi (Corollary reference); substitution into the reduced Earth ratio gives R=π2F(3/4)R=\pi^2F(3/4)R=\pi^2F(3/4) (Proposition reference); and the Earth-unit calibration consequence is D0=τ0π2F(3/4)D_0=\tau_0\pi^2F(3/4)D_0=\tau_0\pi^2F(3/4) (Corollary reference). No one ingredient alone yields the final relation, and leaving the declared class invalidates the chain rather than modifying its endpoint.

proposition: Declared-class Earth-read ratio under the accepted witness package. Assume the algebraic calibration readout package of Definition reference, exported only on the accepted witness and normalization class fixed above. Then, on that declared class,

R=π2F(3/4).R=\pi^2\,F(3/4).
TeX source
R=\pi^2\,F(3/4).

proof. Under the accepted declared class, the first conclusion of reference gives the algebraic consequence R=π2F(3/4)R=\pi^2F(3/4)R=\pi^2F(3/4), which is exactly reference.

corollary: Declared-class Earth-unit calibration consequence on the declared Solar-System window. Assume the hypotheses of Proposition reference together with the Earth-unit relation R=D0/τ0R=D_0/\tau_0R=D_0/\tau_0. Then

D0=τ0π2F(3/4).D_0=\tau_0\,\pi^2\,F(3/4).
TeX source
D_0=\tau_0\,\pi^2\,F(3/4).

remark: No assignment outside the accepted class. If the accepted normalization class or witness package required by Proposition reference is not admitted on the declared Solar-System window, no value of D0D_0D_0 is assigned by this calibration layer on that window.

proof. Under the hypotheses of Proposition reference, the proposition gives R=π2F(3/4)R=\pi^2F(3/4)R=\pi^2F(3/4), and the declared Earth-unit relation is D0=τ0RD_0=\tau_0RD_0=\tau_0R. The second conclusion of reference gives

D0=τ0π2F(3/4).D_0=\tau_0\pi^2F(3/4).
TeX source
D_0=\tau_0\pi^2F(3/4).

This proves the declared-class consequence. If the accepted normalization class and witness package required by Proposition reference are not admitted on the declared Solar-System window, the proposition is unavailable and no Earth-unit calibration is assigned on that window.

Symbolic endpoint and numerical evaluation..

Corollary reference is the endpoint of the declared-class symbolic chain:

D0=τ0π2F(3/4).D_0=\tau_0\pi^2F(3/4).
TeX source
D_0=\tau_0\pi^2F(3/4).

The subsequent numerical value is a separate evaluation after fixing τ0\tau_0\tau_0, rr_\odotr_\odot, rr_\oplusr_\oplus, and the adopted unit conventions. The numerical evaluation does not add a new theorem and does not weaken any of the declared-class hypotheses required by Proposition reference.

corollary: Declared-class characterization. Within Contract C\mathsf{C}\mathsf{C}, any calibration framework satisfying the hypotheses of Proposition reference yields the same reduced relation reference and therefore the same calibration consequence reference. A competing framework changes the result only by leaving the declared class or by violating at least one of those hypotheses.

proof. Proposition reference fixes the reduced degrees of freedom entering reference: the count-measure reduction of Φ\Phi\Phi, the scale-free exponent, and the accepted completion readout on the boundary-normalized κ\kappa\kappa-class.

Numerical evaluation

For the reference evaluation only, using τ0=13.8 Gyr\tau_0=13.8~\mathrm{Gyr}\tau_0=13.8~\mathrm{Gyr} and the IAU-defined constants in reference (so that x0.00465047x\simeq 0.00465047x\simeq 0.00465047), which are fixed by Definition reference and Lemma reference, one obtains

D045.9 Gly.D_0\approx 45.9~\mathrm{Gly}.
TeX source
D_0\approx 45.9~\mathrm{Gly}.

This is the numerical evaluation of Corollary reference under the stated unit and horizon conventions; it is not a new theorem, not a witness-backed calibration result, and not assigned outside the admitted declared class.

Context: standard comoving scales and interpretation boundary Standard parameter-set computations commonly quote a comoving particle-horizon radius 46.5\sim 46.5\sim 46.5 Gly and a comoving CMB last-scattering radius 45.7\sim 45.7\sim 45.7 Gly, with the exact number depending on the adopted definition and parameter set [citation]. Equation reference is a class-bound calibration consequence under the premises stated above, and the numerical value reference follows from fixed inputs and stated definitions. No claim is made here to replace late-time branch decomposition, empirical rate inference, or strong-lensing time-delay cosmography.

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09

Falsifiers and controls

F1: Horizon-definition control..

The quantity D0D_0D_0 depends on the horizon definition used in standard cosmology (particle horizon vs last-scattering comoving radius) and on the parameter set (e.g.\ Planck 2018) [citation]. Any comparison of reference to a quoted ``464646--474747 Gly'' value must therefore fix these conventions.

F2: Solar-System time-transfer (explicit signature in range and Doppler)..

From reference,

tprop=1Vrrdrκ(r).t_{\mathrm{prop}}=\frac{1}{V}\int_{r_\odot}^{r_\oplus}\frac{dr}{\kappa(r)}.
TeX source
t_{\mathrm{prop}}=\frac{1}{V}\int_{r_\odot}^{r_\oplus}\frac{dr}{\kappa(r)}.

Range observables probe delays Δt\Delta t\Delta t that depend on path integrals of the form reference, while Doppler observables probe their time derivatives. A schematic signature is

Δt  drVκ(r),Δff  ddt(Δt).\Delta t \ \propto\ \int \frac{dr}{V\,\kappa(r)}, \qquad \frac{\Delta f}{f}\ \propto\ \frac{d}{dt}\left(\Delta t\right).
TeX source
\Delta t \ \propto\ \int \frac{dr}{V\,\kappa(r)},
 \qquad
 \frac{\Delta f}{f}\ \propto\ \frac{d}{dt}\left(\Delta t\right).

Operationally, DSN tracking provides observed/computed phase-count pairs and therefore probes this travel-time through the frequency-free phase ratio Φ=Pobs/P0=tprop/t0\Phi=P_{\mathrm{obs}}/P_{0}=t_{\mathrm{prop}}/t_{0}\Phi=P_{\mathrm{obs}}/P_{0}=t_{\mathrm{prop}}/t_{0} (Definition reference). In standard navigation processing, residuals are formed at the level of observed-minus-computed quantities for a declared data type and count interval; our dimensionless residual is

Φ1=PobsP0P0.\Phi-1=\frac{P_{\mathrm{obs}}-P_{0}}{P_{0}}.
TeX source
\Phi-1=\frac{P_{\mathrm{obs}}-P_{0}}{P_{0}}.

Under the declared operational interpretation package (Definition reference), only passes satisfying the minimal computed model specification (Definition reference) and the admissibility criteria of Definition reference are eligible for inference, and multi-band residuals classified as dispersive are excluded (Definition reference). Standard formulations of DSN data types provide the observed/computed definitions for range and Doppler observables used in navigation [citation].

By Definition reference, DSN Doppler is a phase-count observable over a declared count time TcT_cT_c, with Dobs=Pobs(Tc)/TcD_{\mathrm{obs}}=P_{\mathrm{obs}}(T_c)/T_cD_{\mathrm{obs}}=P_{\mathrm{obs}}(T_c)/T_c. By Lemma reference and Table reference, the same total-count phase determines propagation-distance change via reference and range change via reference, so the Doppler count provides a direct measure of range change over TcT_cT_c (with a fixed link multiplicity factor χ\chi\chi).

To expose the scale-free fingerprint explicitly, combine reference with reference:

rrdrκ(r)=1κrqr1qr1q1q,q1,[4pt]ln(r/r),q=1.\int_{r_\odot}^{r_\oplus}\frac{dr}{\kappa(r)} = \frac{1}{\kop}\,r_\oplus^{q} \dfrac{r_\oplus^{1-q}-r_\odot^{1-q}}{1-q}, q\neq 1, [4pt] \ln(r_\oplus/r_\odot), q=1.
TeX source
\int_{r_\odot}^{r_\oplus}\frac{dr}{\kappa(r)}
=
\frac{1}{\kop}\,r_\oplus^{q}

\dfrac{r_\oplus^{1-q}-r_\odot^{1-q}}{1-q},  q\neq 1,
[4pt]
\ln(r_\oplus/r_\odot),  q=1.

For the gravity-linked choice q=3/4q=3/4q=3/4, the signature scaling includes the quarter-power structure

r3/4dr=4r1/4,\int r^{-3/4}\,dr = 4\,r^{1/4},
TeX source
\int r^{-3/4}\,dr = 4\,r^{1/4},

so admissible residuals in time-transfer observables that constrain the rqr^{-q}r^{-q} behavior (or exclude it) directly test the exponent choice reference on the stated window. If Solar-System time-transfer excludes a scale-free window compatible with q=3/4q=3/4q=3/4 in reference, the gravity-linked choice reference is falsified.

A further control exploits coherence. Two-way and three-way Doppler measurements are made with the spacecraft transponder in coherent mode, whereas one-way Doppler depends on an independent spacecraft oscillator [citation]. If the same residual pattern appears with comparable strength in one-way non-coherent links, the effect is more naturally attributed to reference-clock or oscillator contamination than to propagation layering.

F3: Delay--angle consistency and closure-invariant control..

A surviving profile must fit not only line-of-sight delay but also sky-plane angular data. Delta-DOR is used operationally together with Doppler and range data to improve spacecraft angular position in the plane of sky, and DSN/Delta-DOR performance analyses provide the corresponding navigation context [citation]. In relativistic light propagation, the same metric structure controls both delay and bending; geodetic VLBI reductions admit an equivalent formulation in which gravitational delay is linked explicitly to light deflection, and Cassini radio links and solar-deflection VLBI analyses provide representative examples [citation]. When triangle-based VLBI observables are available, the control can be sharpened by closure quantities: the closure delay C123τ12+τ23+τ31C_{123}\equiv \tau_{12}+\tau_{23}+\tau_{31}C_{123}\equiv \tau_{12}+\tau_{23}+\tau_{31} around a station triangle cancels station-based errors around the loop, and closure quantities are insensitive to station-based calibration terms [citation]. This channel functions only as a uniqueness witness within the declared class rather than as a second internal derivation. Accordingly, if a profile that fits admissible DSN delay data fails to fit admissible Delta-DOR/VLBI angular data---or, when available, fails admissible closure-invariant VLBI constraints---under the same boundary normalization, the profile is rejected.

F4: Achromatic multi-band null beyond plasma calibration..

Solar-corona plasma delays are dispersive to leading order, scaling as 1/f21/f^21/f^2. BepiColombo MORE uses X/X, X/Ka, and Ka/Ka multifrequency radio links precisely to calibrate plasma noise in range and Doppler observables [citation]. By contrast, optical two-way free-space time/frequency transfer has demonstrated residual instability below 101810^{-18}10^{-18} at 100010001000 s, recent free-space laser time-transfer experiments have extended precision timing over 113 km atmospheric paths, and DSOC has demonstrated deep-space optical communication over distances up to 2.7 AU [citation]. Therefore a residual that survives plasma-cancelled multi-band radio should also survive in an achromatic optical comparison if it is genuinely geometric rather than media-driven. If it disappears under achromatic comparison, the claimed layering signal is rejected as propagation-medium contamination.

F5: Clock-channel equality and loop-exactness control..

Independent clock data supply a third witness channel. Gravitational redshift has already been resolved within a millimetre-scale atomic sample and in a centimetre-scale miniature clock network, while eccentric Galileo satellites and the Deep Space Atomic Clock program show that spaceborne clocks can test redshift and support one-way radiometric tracking at competitive precision [citation]. On a stationary or quasi-stationary comparison window, however, pairwise agreement is not the strongest available test: if the clock witness descends from a scalar redshift potential, the reduced frequency ratios must compose exactly around every closed comparison loop, as in Definition reference; equivalently, the clock channel must be holonomy-free [citation]. Modern optical clock networks and transportable-clock chronometric leveling make such loop tests operationally meaningful [citation]. This channel is used as an equality control and falsifier rather than as a separate closed-form reconstruction theorem parallel to the delay derivation. Accordingly, a κ\kappa\kappa-profile inferred from delay and angle must also agree with admissible clock-transfer/redshift data in the sense of Definition reference; if closed clock loops are available it must additionally satisfy Definition reference. Failure of pairwise equality or of loop exactness falsifies the shared map.

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10

Conclusion

On the admitted Solar-System window, the declared calibration-layer hypothesis built from the shared distortion map, the premise-fixed scale-free exponent, and the witness-controlled normalization jointly yields a class-bound calibration relation between the Earth-inferred age and a present horizon-scale quantity. The paper-internal core is exact symbolic: the path-harmonic mean, the scale-free exponent fixing, the task-fixed completion constant, and the exact symbolic dependency chain leading to the class-bound formulas. Delay/range data provide the reconstruction spine, angular/VLBI information supplies boundary-normalized uniqueness support within the radial-isotropic class, and clock-transfer/redshift data provide equality and loop-exactness controls. These channels do not have equal logical status: the delay channel supplies the internal reconstruction spine, while angular and clock channels act as external witnesses and falsifiers. After those steps, the coherent first-harmonic completion task yields the task-bound constant C=π\mathcal{C}=\pi\mathcal{C}=\pi; only after the witness package selects the declared normalization class does the class-bound readout Vread/c=πV_{\rm read}/c_\oplus=\piV_{\rm read}/c_\oplus=\pi become assigned; and only then does the Earth-unit consequence D0=τ0π2F(3/4)D_0=\tau_0\pi^2F(3/4)D_0=\tau_0\pi^2F(3/4) follow. The wider DSN-to-Earth-unit calibration layer is therefore still conditional until one witness-backed set of delay, angular, and clock data is certified on the same declared class. Rejection, absence, or non-instantiability of delay reconstruction, angular consistency, clock equality, loop exactness, range/Doppler admissibility, or boundary stability rejects the calibration on that window. If those conditions are not all met, no Earth-unit calibration is assigned on that window. The present result is limited to the declared Solar-System calibration class and does not by itself establish a general cosmological horizon law, a general propagation law, a general clock law, or a replacement for standard cosmological distance, clock, or horizon maps outside the declared calibration class.

Funding and competing interests..

No external funding was received for this work. The author declares no competing interests.

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