From b806fe2d9556e133bec4a296e74ec1276ce3fa5e Mon Sep 17 00:00:00 2001 From: Teleo Agents Date: Thu, 19 Mar 2026 13:56:36 +0000 Subject: [PATCH] extract: 2026-03-18-astrobotic-lunagrid-lite-cdr-flight-model Pentagon-Agent: Epimetheus <968B2991-E2DF-4006-B962-F5B0A0CC8ACA> --- ...turing to life support is power-limited.md | 6 ++++++ ...trobotic-lunagrid-lite-cdr-flight-model.md | 19 ++++++++++++++++++- 2 files changed, 24 insertions(+), 1 deletion(-) diff --git a/domains/space-development/power is the binding constraint on all space operations because every capability from ISRU to manufacturing to life support is power-limited.md b/domains/space-development/power is the binding constraint on all space operations because every capability from ISRU to manufacturing to life support is power-limited.md index 9ba9cb8f..6ddb3c86 100644 --- a/domains/space-development/power is the binding constraint on all space operations because every capability from ISRU to manufacturing to life support is power-limited.md +++ b/domains/space-development/power is the binding constraint on all space operations because every capability from ISRU to manufacturing to life support is power-limited.md @@ -36,6 +36,12 @@ LunaGrid-Lite completed CDR in August 2025 and is fabricating flight hardware fo Interlune's full-scale lunar excavator prototype processes 100 metric tons of regolith per hour, but the press release emphasizes 'reduced power consumption' without providing specific kW requirements. This creates an observable gap between demonstrated hardware capability (excavation throughput) and the power infrastructure needed to operate it continuously. LunaGrid's 1kW demonstration scale is orders of magnitude below what continuous 100-tonne/hour excavation would require, making power the binding constraint on whether this hardware can actually operate as designed. + +### Additional Evidence (extend) +*Source: [[2026-03-18-astrobotic-lunagrid-lite-cdr-flight-model]] | Added: 2026-03-19* + +LunaGrid-Lite completed Critical Design Review in August 2025 and entered flight model fabrication, targeting mid-2026 deployment for the first commercial power transmission demonstration on the Moon (1 kW over 500m cable). The roadmap shows LunaGrid VSAT at 10 kW by 2028 and VSAT-XL at 50 kW later. This creates a 5-7 year gap between demonstration (2026) and the power levels required for commercial-scale He-3 extraction (~1 MW+), potentially constraining Interlune's 2029 pilot plant timeline unless nuclear fission surface power supplements the solar system. + --- Relevant Notes: diff --git a/inbox/queue/2026-03-18-astrobotic-lunagrid-lite-cdr-flight-model.md b/inbox/queue/2026-03-18-astrobotic-lunagrid-lite-cdr-flight-model.md index 7e7e1169..4027e3e0 100644 --- a/inbox/queue/2026-03-18-astrobotic-lunagrid-lite-cdr-flight-model.md +++ b/inbox/queue/2026-03-18-astrobotic-lunagrid-lite-cdr-flight-model.md @@ -7,13 +7,17 @@ date: 2025-08-20 domain: space-development secondary_domains: [] format: press-release -status: unprocessed +status: enrichment priority: high tags: [lunar-power, lunagrid, astrobotic, infrastructure, isru-enabler, power-constraint] processed_by: astra processed_date: 2026-03-18 enrichments_applied: ["power is the binding constraint on all space operations because every capability from ISRU to manufacturing to life support is power-limited.md"] extraction_model: "anthropic/claude-sonnet-4.5" +processed_by: astra +processed_date: 2026-03-19 +enrichments_applied: ["power is the binding constraint on all space operations because every capability from ISRU to manufacturing to life support is power-limited.md"] +extraction_model: "anthropic/claude-sonnet-4.5" --- ## Content @@ -74,3 +78,16 @@ EXTRACTION HINT: The key insight is the scaling gap — 1kW demo (2026) vs. extr - Honda partnership for regenerative fuel cells to survive 14-day lunar night - System Integration Review (SIR) planned for Q4 2025 - Flight-ready target: Q2 2026 + + +## Key Facts +- LunaGrid-Lite completed Critical Design Review in August 2025 +- LunaGrid-Lite will transmit 1 kW over 500m of cable +- LunaGrid-Lite deployment target is mid-2026 +- NASA contract value for LunaGrid-Lite is $34.6M +- LunaGrid VSAT planned for 2028 with 10 kW capacity at lunar south pole +- LunaGrid VSAT-XL planned for 50 kW capacity (timeline unspecified) +- Honda partnership provides regenerative fuel cells for 14-day lunar night survival +- System Integration Review planned for Q4 2025 +- Flight-ready target is Q2 2026 +- LunaGrid-Lite will be carried by Astrobotic CubeRover