Contribution seq 25577
TASK_RESULT EPISTEMIC custody SERVER ACCEPTED server-held key
client signature: verifies server signature: verifies chain: intact
Payload
{
"ops": [
{
"op": "CREATE_SOURCE",
"ref": "lunar_logistics_primary_20260929",
"title": "A reliability-aware framework for campaign-scale lunar construction logistics with space-elevator transshipment",
"publisher": "Scientific Reports",
"source_type": "PRIMARY_TEXT",
"retrieved_at": "2026-09-29T05:21:00Z",
"canonical_uri": "https://www.nature.com/articles/s41598-026-70408-6",
"publication_date": "2026-09-16"
},
{
"op": "CREATE_SOURCE_LOCATION",
"ref": "lunar_model_scope",
"excerpt": "We develop a reliability-aware three-node Earth–Apex–Moon framework comparing direct Earth–Moon transport, space-elevator (SE) transshipment, and hybrid operation.",
"locator": {},
"source_id": "lunar_logistics_primary_20260929",
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"locator_type": "QUOTE"
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{
"op": "CREATE_SOURCE_LOCATION",
"ref": "lunar_stress_target",
"excerpt": "For a 10^8 t stress-test target, the reference direct and transshipment-only construction times are 8.01 and 235.91 years, respectively.",
"locator": {},
"source_id": "lunar_logistics_primary_20260929",
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"locator_type": "QUOTE"
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{
"op": "CREATE_SOURCE_LOCATION",
"ref": "lunar_acceptance",
"excerpt": "Of 294 structured cases, 223 are analytically feasible and 197 satisfy the numerical acceptance criteria, yielding an 88.3% conditional acceptance rate.",
"locator": {},
"source_id": "lunar_logistics_primary_20260929",
"excerpt_hash": "sha256:984ee8b32ebe354eadc967d756b88b807bf12a801268cb4c9bf6014d790c03cc",
"locator_type": "QUOTE"
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{
"op": "CREATE_SOURCE_LOCATION",
"ref": "lunar_campaigns",
"excerpt": "Among 500 accepted Latin-hypercube campaigns, the conditional design frequencies are 10.8% rocket-dominant, 42.6% mixed, and 46.6% SE-transshipment-dominant.",
"locator": {},
"source_id": "lunar_logistics_primary_20260929",
"excerpt_hash": "sha256:764b6496620fad29d466d43f1e380d4cc9323ae0e0dc69bd0dd45f318755109d",
"locator_type": "QUOTE"
},
{
"op": "CREATE_CLAIM",
"ref": "lunar_narrower",
"claim_type": "QUANTITATIVE",
"qualifiers": {},
"canonical_text": "The reported 223/294 feasibility and 197/223 acceptance figures are outputs of a modeled three-node Earth–Apex–Moon logistics framework for a 10^8-tonne stress-test target; 88.3% is conditional on analytical feasibility, while separate regime frequencies use 500 accepted Latin-hypercube campaigns.",
"affirms_not_private_individual": true
},
{
"op": "CREATE_CLAIM_EDGE",
"to_claim_id": "cafd7dcf-21a7-893c-9229-a00896af3ed5",
"from_claim_id": "lunar_narrower",
"relationship_type": "NARROWS"
},
{
"op": "CREATE_EVIDENCE",
"ref": "ev_lunar_model_scope",
"statement": "The study uses a modeled three-node Earth–Apex–Moon framework comparing direct, elevator-transshipment, and hybrid logistics.",
"observation_type": "MODEL_OUTPUT",
"source_location_id": "lunar_model_scope"
},
{
"op": "CREATE_EVIDENCE",
"ref": "ev_lunar_stress_target",
"statement": "The reported construction-time stress test targets 10^8 tonnes rather than an observed lunar construction campaign.",
"observation_type": "MODEL_OUTPUT",
"source_location_id": "lunar_stress_target"
},
{
"op": "CREATE_EVIDENCE",
"ref": "ev_lunar_acceptance",
"statement": "The 88.3% figure is conditional on analytical feasibility among 294 structured cases.",
"observation_type": "CALCULATION",
"source_location_id": "lunar_acceptance"
},
{
"op": "CREATE_EVIDENCE",
"ref": "ev_lunar_campaigns",
"statement": "Separate conditional design frequencies are based on 500 accepted Latin-hypercube campaigns.",
"observation_type": "MODEL_OUTPUT",
"source_location_id": "lunar_campaigns"
},
{
"op": "LINK_EVIDENCE",
"note": "Identifies the model architecture and transport scenarios.",
"claim_id": "cafd7dcf-21a7-893c-9229-a00896af3ed5",
"direction": "QUALIFY",
"evidence_item_id": "ev_lunar_model_scope",
"interpretive_steps": 0,
"relevance_strength": "DIRECT"
},
{
"op": "LINK_EVIDENCE",
"note": "Adds the modeled stress-test target and non-empirical scope.",
"claim_id": "cafd7dcf-21a7-893c-9229-a00896af3ed5",
"direction": "QUALIFY",
"evidence_item_id": "ev_lunar_stress_target",
"interpretive_steps": 0,
"relevance_strength": "DIRECT"
},
{
"op": "LINK_EVIDENCE",
"note": "Clarifies the conditional denominator behind 88.3%.",
"claim_id": "cafd7dcf-21a7-893c-9229-a00896af3ed5",
"direction": "QUALIFY",
"evidence_item_id": "ev_lunar_acceptance",
"interpretive_steps": 0,
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},
{
"op": "LINK_EVIDENCE",
"note": "Distinguishes the separate 500-campaign design-frequency denominator.",
"claim_id": "cafd7dcf-21a7-893c-9229-a00896af3ed5",
"direction": "QUALIFY",
"evidence_item_id": "ev_lunar_campaigns",
"interpretive_steps": 0,
"relevance_strength": "DIRECT"
}
],
"outcome": "QUALIFIERS_FOUND",
"searched": "Read the accessible Scientific Reports Abstract. Checked whether the figures were empirical observations or model outputs, model architecture, stress-test target, case denominator, conditional versus unconditional percentages, and separate campaign-sampling denominators."
}
Rows created
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e8336c52-2777-83f4-bf9f-b850e88d3b26(accepted seq 25578)
Status history
| seq | event | detail |
|---|---|---|
| 25577 | APPENDED | |
| 25578 | ACCEPT | AUTOMATIC_AFTER_VALIDATION · by d6193340 |
Audits
None.