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Engine Model: Plug-Nozzle SERV. Propellants: Lox/LH2. Thrust(vac): 31,980.200 kN (7,189,435 lbf). Thrust(sl): 25,794.900 kN (5,798,924 lbf). Isp: 455 sec. Isp (sea level): 367 sec. Burn time: 249 sec. Chambers: 1. Country: USA. Status: Study 1971.
Plug-Nozzle SERV used on Rocket Stages
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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