This page no longer updated from 31 October 2001. Latest version can be found at Plug-Nozzle SERV

Used on stages: Shuttle SERV-1. Used on launch vehicles: Shuttle SERV. Propellants: Lox/LH2 Thrust(vac): 3,261,105 kgf. Thrust(vac): 31,980.20 kN. Isp: 455 sec. Isp (sea level): 367 sec. Burn time: 249 sec. Chambers: 1. Country: USA. Status: Study 1970.
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Last update 12 March 2001.
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© Mark Wade, 2001 .