extract: 2026-03-19-spacex-starship-b19-static-fire-anomaly
Some checks are pending
Sync Graph Data to teleo-app / sync (push) Waiting to run
Some checks are pending
Sync Graph Data to teleo-app / sync (push) Waiting to run
Pentagon-Agent: Epimetheus <3D35839A-7722-4740-B93D-51157F7D5E70>
This commit is contained in:
parent
d059e62072
commit
1b35f6146e
2 changed files with 24 additions and 1 deletions
|
|
@ -37,6 +37,12 @@ Starship V3 demonstrates 3x payload capacity jump (35t to 100+ tonnes LEO) with
|
|||
|
||||
Starship V3 specifications show 100+ tonnes to LEO payload capacity (vs. ~35t for V2), representing a 3x payload increase. With 33 Raptor 3 engines at ~280 tonnes thrust each (22% more than Raptor 2) and 2,425 lbs lighter per engine, the V3 vehicle increases the payload denominator by 3x independent of reuse rate improvements. Flight 12 in April 2026 will be the first empirical test of these specifications. The 3x payload jump means fixed costs (vehicle amortization, ground operations, regulatory) are spread over 3x more mass, driving $/kg down proportionally even before cadence improvements.
|
||||
|
||||
|
||||
### Additional Evidence (challenge)
|
||||
*Source: [[2026-03-19-spacex-starship-b19-static-fire-anomaly]] | Added: 2026-03-20*
|
||||
|
||||
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.
|
||||
|
||||
---
|
||||
|
||||
Relevant Notes:
|
||||
|
|
|
|||
|
|
@ -7,9 +7,13 @@ date: 2026-03-19
|
|||
domain: space-development
|
||||
secondary_domains: []
|
||||
format: news
|
||||
status: unprocessed
|
||||
status: enrichment
|
||||
priority: medium
|
||||
tags: [starship, spacex, raptor3, v3, static-fire, flight-12, launch-cost, keystone-variable, delay-risk]
|
||||
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"]
|
||||
extraction_model: "anthropic/claude-sonnet-4.5"
|
||||
---
|
||||
|
||||
## Content
|
||||
|
|
@ -63,3 +67,16 @@ All four must clear before launch. The April 9 target was always aggressive; thi
|
|||
PRIMARY CONNECTION: [[Starship achieving routine operations at sub-100 dollars per kg is the single largest enabling condition for the entire space industrial economy]] — this is an update to the timeline and risk profile
|
||||
WHY ARCHIVED: Static fire anomaly on the day before research date is material new information for the Flight 12 risk profile; the April 9 target is now more uncertain
|
||||
EXTRACTION HINT: Do not extract a claim from this alone — pair with the Flight 12 result when available. The claim to update is the keystone variable enabler claim, once V3 specs are empirically validated or modified.
|
||||
|
||||
|
||||
## Key Facts
|
||||
- Starship Booster 19 conducted a 10-engine static fire test on March 19, 2026 that ended abruptly
|
||||
- The anomaly was ground-side (OLP-2 infrastructure), not engine-related
|
||||
- SpaceX is preparing for a 33-engine static fire test of B19
|
||||
- Flight 12 target date is NET April 9, 2026 at 5:30pm CST
|
||||
- FAA had not granted Flight 12 launch license as of late January 2026
|
||||
- Ship 39 is separately moving through preflight test objectives
|
||||
- Raptor 3 engines produce ~280 tonnes thrust each (22% more than Raptor 2)
|
||||
- Raptor 3 engines are 2,425 lbs lighter per engine than Raptor 2
|
||||
- V3 target payload capacity is 100+ tonnes to LEO vs ~35 tonnes for V2 non-reusable
|
||||
- Flight 12 will launch from new Orbital Launch Pad 2 (OLP-2)
|
||||
|
|
|
|||
Loading…
Reference in a new issue