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Shuttle SERV-1
LOx/LH2 propellant rocket stage. Single stage to orbit, ballistic reentry.

AKA: Shuttle SERV. Status: Study 1971. Thrust: 31,980.52 kN (7,189,506 lbf). Gross mass: 2,040,816 kg (4,499,229 lb). Unfuelled mass: 226,757 kg (499,913 lb). Specific impulse: 455 s. Specific impulse sea level: 367 s. Burn time: 249 s. Height: 20.27 m (66.50 ft). Diameter: 18.29 m (60.00 ft). Span: 27.44 m (90.02 ft).



Country: USA. Engines: Plug-Nozzle SERV. Launch Vehicles: SERV. Propellants: Lox/LH2.

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