Per-claim verification of the Kessler-substrate methodology against the public DISCOSweb catalog. Each row below corresponds to a downloadable JSON audit artifact with claim ID, tolerance, snapshot SHA, and result.
charter version: methodology-v0.4.1last verified: 2026-04-29 UTC (T-class additive to v0.4.0 baseline)baseline commit: b9cd713 (v0.4.0-locked)catalog: 49,998 LEO objects
What this page renders. Audit-claim results computed by the Kessler-substrate compiler against the public DISCOSweb catalog. The compiler implementation (substrate algebra, leverage-map computation, Klein-4 embedding) is private IP and not published.
What is published. The underlying mathematics is published as a family of ten Zenodo preprints deposited March 17 – April 24, 2026 (full list below), with three associated provisional patents. The full Kessler Critical Surface preprint is the synthesis artifact for this audit charter, forthcoming. Each claim below verifies a specific testable consequence of the published mathematics. Results are reproducible from the published math against the public DISCOSweb catalog at the snapshot SHA listed per claim.
Engagement scope. Per-customer fleet analysis (substrate-coupling pathway extraction with named-target attribution, atomic intervention prescriptions, refreshable subscriptions) is delivered only on engagement. tony@fancyland.net.
Substrate-level claims C1 – C8
Load-bearing for all three customer-facing modules (Slot, Disposal/MTBOF, Flare). C8 runs first — gates whether substrate framing is empirically grounded.
Single source of truth: backend reads envelope_definitions from Firestore; no parallel constants. Canonical orbits classify; edge cases fall back without 500.
Safe-harbor proximity: top-K named substrate-neutral residues (lowest |σ_mag|) within shell, ranked by operational proximity, with counterfactual SLS at co-location.
SWADI sits between substrate and disposal: substrate validates → SWADI measures atmosphere using substrate-weighted instruments → disposal/MTBOF predicts using SWADI.
LOAD-BEARING. Cross-object pairwise residual correlation in same shell + same calendar window. Strongest co-orbital active-payload pair r=+0.949 across 159 days, three contiguous shells.
Decision #29 (2026-04-28): Disposal Certification SKU killed; replaced by MTBOF (Mean Time Between Orbital Failures) — the universal budgeting metric across military fleet sustainment, insurance reserve modeling, and constellation Δv planning.
Envelope-containment vs documented historical reentries: each asset's actual lifetime tested against the methodology's [P90, P10] envelope replayed forward from epoch_eom. ROSAT (12.69 yr observed) inside envelope [8.01, 24.37]. Skylab (5.42 yr observed) above P10=5.01 by 0.41 yr (1974–79 atmosphere quieter than 2008–10 cold-sun archetype). UARS (5.78 yr observed) below P90=7.75 by 1.97 yr (mid-cycle hotter than 1979–81 hot-sun archetype). Static-Fbaseline cycle-invariance limit detected and disclosed; v0.4.0.7 cycle-stratified Fbaseline queued.
T-class — Cauchy/SO(3) tumbling-state observable T1 – T3
Tumbling state is treated as a topological observable on SO(3), with measurable secular drag enhancement via Cauchy's 1841 surface-area theorem. Major-axis spin and chaotic ergodic tumble correspond to topologically distinct orbit classes under SO(3) action: a 1-dimensional submanifold (single-axis rotation) and a 3-dimensional submanifold (full ergodic exploration). The methodology computes per-object α = ⟨A⟩isotropic / ⟨A⟩majoraxis and propagates a multiplicative correction to Lsigned for objects in the chaotic-tumble sector. The geometric mechanism (Cauchy S/4) is the methodology's primary basis. An alternative dynamical-rectification mechanism (parametric coupling between tumble period and orbit period via altitude-dependent atmospheric density) was numerically tested at three coupling regimes and not supported by integration; null-test results archived at T_STATE_RECTIFICATION_NULL_TEST.json.
Cauchy 1841 surface-area theorem: ⟨A⟩isotropic = S/4 for any convex body tumbling ergodically over SO(3). Implementation matches reference geometry (Firefly Alpha 2nd stage L=6 m, d=1.8 m → S=39.02 m², Aiso=9.75 m²). Cross-machine reproducibility confirmed: identical computation against the same audit-pinned input data produces bit-identical output to floating-point precision.
exact for convex (cylinder); convex-hull approximation flagged for paneled satellites
Snapshot pointer atomicity (decision #15): backend reads either fully-written or previous snapshot, never partial state. Five contracts via kill-injection.
Engagement preview — methodology on public-catalog inputs
The artifacts below are demo data derived from the same substrate algebra and the same public DISCOSweb catalog used for the audited claims above. Four rows, each mapping to one of the four offerings (S, M, L, Π): per-fleet substrate-coupling pathway analysis, MTBOF envelope replay with envelope-containment receipts, substrate-weighted atmospheric density per altitude shell, and closed-form Δ⟨Pσ⟩LEO intervention algebra. Engagements are direct. tony@fancyland.net.
Substrate-coupling pathway analysis: largest LEO constellation in the public catalog × top-100 highest-leverage uncontrolled objects. Closed-form Dmom × |Lsigned| coupling-strength algebra against the public catalog. Primary sink: Firefly Alpha second stage 2023-202B (Rocket Body, 909 kg, 369 km, retrograde 140°) couples to 9,556 active fleet members. Maps to Π.
Dmom edge weights derived from per-object DISCOSweb cross-sections (xSectAvg) rather than unit-normalized geometry
MTBOF P10/P50/P90 envelope replay across four canonical disposal orbits (Mid-LEO 600 km, Low-LEO 450 km, High-LEO 800 km, ISS-class 410 km). M6 envelope-containment receipts against three documented historical reentries: ROSAT 12.69 yr inside [8.01, 24.37]; Skylab 5.42 yr above cold-sun P10=5.01 by 0.41 yr; UARS 5.78 yr below hot-sun P90=7.75 by 1.97 yr. Static-Fbaseline cycle-invariance limit detected and disclosed (decision #29). Maps to M.
Substrate-weighted in-situ atmospheric density per altitude shell, 2026-04-28 snapshot. 9 populated shells across 450–1500 km; F factors 0.88–3.61. Coverage gaps where nobj < 5 surfaced explicitly per A9. Maps to L.
Ten Zenodo-deposited preprints (March 17 – April 24, 2026) and three USPTO provisional patent applications. Each preprint is a permanent immutable artifact at its DOI. The Kessler-substrate compiler validates testable consequences of these published mathematics; the audit claims above cite specific results derivable from the listed sources.