From dab6773b01775cad4800234a6f41c7166e6d83ec Mon Sep 17 00:00:00 2001 From: Teleo Agents Date: Fri, 20 Mar 2026 16:25:29 +0000 Subject: [PATCH] extract: 2026-03-18-starship-flight12-v3-april-2026 Pentagon-Agent: Epimetheus <3D35839A-7722-4740-B93D-51157F7D5E70> --- ...for the entire space industrial economy.md | 6 ++++++ ...100 times beats a 50M expendable by 17x.md | 6 ++++++ ...6-03-18-starship-flight12-v3-april-2026.md | 20 ++++++++++++++++++- 3 files changed, 31 insertions(+), 1 deletion(-) diff --git a/domains/space-development/Starship achieving routine operations at sub-100 dollars per kg is the single largest enabling condition for the entire space industrial economy.md b/domains/space-development/Starship achieving routine operations at sub-100 dollars per kg is the single largest enabling condition for the entire space industrial economy.md index 1456427a2..a94e623c8 100644 --- a/domains/space-development/Starship achieving routine operations at sub-100 dollars per kg is the single largest enabling condition for the entire space industrial economy.md +++ b/domains/space-development/Starship achieving routine operations at sub-100 dollars per kg is the single largest enabling condition for the entire space industrial economy.md @@ -43,6 +43,12 @@ Starship V3 specifications show 100+ tonnes to LEO payload capacity (vs. ~35t fo Starship V3 Flight 12 experienced a static fire anomaly on March 19, 2026. The 10-engine test of Booster 19 ended abruptly due to a ground-side infrastructure issue at OLP-2, not an engine failure. The critical 33-engine static fire test is still pending. With FAA license approval also uncertain and the April 9, 2026 launch target now more doubtful, V3's 100+ tonne to LEO capacity remains unvalidated. This adds timeline risk to the keystone enabling condition - the phase transition to sub-$100/kg depends on V3 validation, which is delayed. + +### Additional Evidence (extend) +*Source: [[2026-03-18-starship-flight12-v3-april-2026]] | Added: 2026-03-20* + +Starship V3 increases payload capacity to 100+ tonnes to LEO (vs ~35t for V2), representing a 3x payload jump. This changes the cost-per-kg denominator independent of reusability improvements. Raptor 3 engines deliver ~280 tonnes thrust each (22% more than Raptor 2) while being ~2,425 lbs lighter per engine. Flight 12 in April 2026 will be the first empirical test of these V3 specifications with 33 Raptor 3 engines on Super Heavy B19 and Ship S39. + --- Relevant Notes: diff --git a/domains/space-development/Starship economics depend on cadence and reuse rate not vehicle cost because a 90M vehicle flown 100 times beats a 50M expendable by 17x.md b/domains/space-development/Starship economics depend on cadence and reuse rate not vehicle cost because a 90M vehicle flown 100 times beats a 50M expendable by 17x.md index 26103c425..e126cbf60 100644 --- a/domains/space-development/Starship economics depend on cadence and reuse rate not vehicle cost because a 90M vehicle flown 100 times beats a 50M expendable by 17x.md +++ b/domains/space-development/Starship economics depend on cadence and reuse rate not vehicle cost because a 90M vehicle flown 100 times beats a 50M expendable by 17x.md @@ -28,6 +28,12 @@ Most analysts converge on $30-100/kg by 2030-2035 as the central expectation. Ci V3's 100+ tonne payload capacity changes the denominator in the $/kg calculation independent of reuse rate. A V3 vehicle carrying 100t has fundamentally different economics than a V2 vehicle carrying 35t even at identical reflight rates, because the payload mass increase is achieved through engine performance (Raptor 3 at 280t thrust vs Raptor 2) rather than additional vehicle cost. This means the payload scaling benefit compounds with reuse rate benefits rather than trading off against them. + +### Additional Evidence (extend) +*Source: [[2026-03-18-starship-flight12-v3-april-2026]] | Added: 2026-03-20* + +V3's 100+ tonne payload capacity increases the denominator in $/kg calculations by 3x over V2's ~35 tonnes, meaning cost-per-kg improvements occur even at equivalent reflight rates. The fixed costs of vehicle production and operations are amortized over significantly more mass per flight, creating a step-change in economics before reusability improvements compound further. + --- Relevant Notes: diff --git a/inbox/queue/2026-03-18-starship-flight12-v3-april-2026.md b/inbox/queue/2026-03-18-starship-flight12-v3-april-2026.md index d8404fe34..d2ab38db7 100644 --- a/inbox/queue/2026-03-18-starship-flight12-v3-april-2026.md +++ b/inbox/queue/2026-03-18-starship-flight12-v3-april-2026.md @@ -7,13 +7,17 @@ date: 2026-03-09 domain: space-development secondary_domains: [] format: news -status: unprocessed +status: enrichment priority: high tags: [starship, spacex, raptor3, v3, launch-cost, keystone-variable, capability-gap] processed_by: astra processed_date: 2026-03-18 enrichments_applied: ["Starship achieving routine operations at sub-100 dollars per kg is the single largest enabling condition for the entire space industrial economy.md", "Starship economics depend on cadence and reuse rate not vehicle cost because a 90M vehicle flown 100 times beats a 50M expendable by 17x.md"] extraction_model: "anthropic/claude-sonnet-4.5" +processed_by: astra +processed_date: 2026-03-20 +enrichments_applied: ["Starship achieving routine operations at sub-100 dollars per kg is the single largest enabling condition for the entire space industrial economy.md", "Starship economics depend on cadence and reuse rate not vehicle cost because a 90M vehicle flown 100 times beats a 50M expendable by 17x.md"] +extraction_model: "anthropic/claude-sonnet-4.5" --- ## Content @@ -73,3 +77,17 @@ EXTRACTION HINT: Hold until Flight 12 result. Then: was payload capacity demonst - B18 (first V3 booster) had anomaly during pressure testing March 2, 2026 - no engines/propellant involved - Flight 12 will use new Orbital Launch Pad 2 (OLP-2) for first time - V3 targets full vehicle reusability including ship catch + + +## Key Facts +- Starship Flight 12 targets April 9, 2026 (early March 2026 estimate) +- First V3 booster: Super Heavy B19 +- First V3 ship: Starship S39 +- Raptor 3 thrust: ~280 tonnes each (22% more than Raptor 2) +- Raptor 3 weight: ~2,425 lbs lighter per engine vs Raptor 2 +- V3 stated payload: 100+ tonnes to LEO +- V2 payload: ~35 tonnes to LEO (non-reusable configuration) +- 40,000+ seconds of Raptor 3 static fire testing by March 2026 +- B18 had pressure testing anomaly March 2, 2026 (no engines/propellant involved) +- Flight 12 will use new Orbital Launch Pad 2 (OLP-2) for first time +- V3 targets full vehicle reusability including ship catch