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ArmorandClaude Opus 4.7 3cfbf8433d docs: update Vulture Shuttle wiki — RS-25EX specs, abort modes, booster engine-out
- Replace RS-25E with RS-25EX throughout (2.88 t, 26 MPa, 2812 kN, 454 s vac / 2353.7 kN, 380 s SL)
- Dry mass 111.6 t → 110.5 t; burn time 10m16s → 8m30s normal / 12m extended
- Rewrite abort section: 6 modes (add Hard Abort), detailed main engine engine-out
  scenario (100 t to 650×650 km, 28° from Wenchang)
- Add booster engine-out section (TH-12 tolerance, downrange/recovery abort, T+60s
  worst case → RTLS / Hard Abort)
- Fix ST-02 reference: 万星源NEXT号 → 克丽斯腾号

Co-Authored-By: Claude Opus 4.7 <noreply@anthropic.com>
2026-06-05 16:19:11 +08:00
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