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:

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:

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