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Shuttle FR-3-2
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Gross Mass: 388,189 kg (855,810 lb). Empty Mass: 130,159 kg (286,951 lb). Thrust (vac): 4,549.049 kN (1,022,667 lbf). Isp: 459 sec. Burn time: 251 sec. Propellants: Lox/LH2. Isp(sl): 359 sec. Diameter: 7.46 m (24.47 ft). Span: 21.75 m (71.35 ft). Length: 54.57 m (179.03 ft). Country: USA. No Engines: 2. Engine: SSME Study. Status: Study 1969. First Flight: 1978. Trapezoidal lifting body configuration. Cross range 2419 km.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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