57 lines
3.7 KiB
Markdown
57 lines
3.7 KiB
Markdown
---
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type: source
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title: "Starship Flight 12: First V3 Vehicles with Raptor 3, Targeting April 2026"
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author: "NASASpaceFlight / Tesla Oracle / SpaceX"
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url: https://www.nasaspaceflight.com/2025/12/flight-12-vehicles-2026/
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date: 2026-03-09
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domain: space-development
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secondary_domains: []
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format: news
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status: unprocessed
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priority: high
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tags: [starship, spacex, raptor3, v3, launch-cost, keystone-variable, capability-gap]
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---
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## Content
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Starship Flight 12 is targeting April 2026 (approximately April 9 per early March 2026 estimates). This will be the first flight of Block 3 (V3) Starship vehicles.
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**V3 hardware specifications:**
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- Booster: Super Heavy B19 (first V3 booster)
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- Ship: Starship S39 (first V3 ship)
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- Engines: 33 Raptor 3 engines on booster
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- Raptor 3 thrust: ~280 tonnes each (22% more than Raptor 2), ~2,425 lbs lighter per engine
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- Stated payload: 100+ tonnes to LEO (vs. ~35t for V2 in non-reusable configuration)
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- Launch pad: New Orbital Launch Pad 2 (OLP-2) — first use
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**Program context:**
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- 40,000+ seconds of Raptor 3 static fire testing accumulated
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- B18 (first V3 booster) had anomaly during pressure testing March 2 — but no engines/propellant involved
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- V3 target: full vehicle reusability including ship catch (Mechazilla booster catch already demonstrated)
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- Ship 39 preparing for rollout
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**What this launch tests:**
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1. Raptor 3 performance at scale (33 engines in flight configuration)
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2. V3 vehicle structural improvements
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3. New OLP-2 infrastructure
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4. V3 ship ocean landing capability (precursor to ship catch)
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## Agent Notes
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**Why this matters:** Starship V3 at 100+ tonnes to LEO is the specific capability level referenced in my keystone belief. The 3x payload jump over V2 (~35t) activates different economics — if V3 achieves routine operations at this capacity, it changes the math for LEO commercial stations, propellant depots, and lunar cargo transport. Flight 12 is the validation test for these specs.
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**What surprised me:** The 3x payload jump between V2 and V3 is larger than I expected — this is not incremental iteration but a significant capability step change. If Raptor 3 performs as specified, the cost-per-kg drops further even before reusability improvements, because the fixed costs are amortized over more mass.
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**What I expected but didn't find:** Cost-per-kg estimates for Starship V3 vs. V2. SpaceX doesn't publish these, but the 3x payload increase should roughly halve the $/kg cost at equivalent reflight rates.
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**KB connections:**
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- [[Starship achieving routine operations at sub-100 dollars per kg is the single largest enabling condition for the entire space industrial economy]] — V3 flight is the first empirical test of the V3 vehicle that enables this
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- [[Starship economics depend on cadence and reuse rate not vehicle cost because a 90M vehicle flown 100 times beats a 50M expendable by 17x]] — V3's 100t payload changes the denominator in the $/kg calculation
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**Extraction hints:**
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- When flight result is known: update claim on Starship V3 capability with first-flight data
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- New claim candidate if V3 performs: "Starship V3 at 100+ tonnes to LEO increases the payload denominator 3x over V2, driving $/kg down by a comparable factor independent of reuse rate improvements"
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## Curator Notes
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PRIMARY CONNECTION: [[Starship achieving routine operations at sub-100 dollars per kg is the single largest enabling condition for the entire space industrial economy]]
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WHY ARCHIVED: First V3 flight is the empirical test of the keystone variable enabler; result will determine whether V3 spec claims are validated or need revision
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EXTRACTION HINT: Hold until Flight 12 result. Then: was payload capacity demonstrated? Did Raptor 3 achieve expected thrust? Update the $/kg cost curve calculation if data is available.
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