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Shuttle HCR-1
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Gross Mass: 1,634,467 kg (3,603,382 lb). Empty Mass: 304,535 kg (671,384 lb). Thrust (vac): 29,135.625 kN (6,549,949 lbf). Isp: 442 sec. Burn time: 195 sec. Propellants: Lox/LH2. Isp(sl): 392 sec. Diameter: 10.00 m (32.00 ft). Span: 46.04 m (151.04 ft). Length: 70.79 m (232.25 ft). Country: USA. No Engines: 14. Engine: SSME Study. Status: Study 1969. First Flight: 1978. Swept wing configuration.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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