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Shuttle HCR-2
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Gross Mass: 342,948 kg (756,070 lb). Empty Mass: 129,329 kg (285,121 lb). Thrust (vac): 4,719.636 kN (1,061,016 lbf). Isp: 459 sec. Burn time: 201 sec. Propellants: Lox/LH2. Isp(sl): 359 sec. Diameter: 7.50 m (24.60 ft). Span: 29.73 m (97.53 ft). Length: 48.26 m (158.33 ft). Country: USA. No Engines: 2. Engine: SSME Study. Status: Study 1969. First Flight: 1978. Delta winged configuration.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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