This page no longer updated from 31 October 2001.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

Used on stages: SASSTO. Used on launch vehicles: SASSTO. Propellants: Lox/LH2 Thrust(vac): 160,600 kgf. Thrust(vac): 1,574.90 kN. Isp: 459 sec. Isp (sea level): 359 sec. Burn time: 268 sec. Chambers: 1. Country: USA. Status: Study 1966.
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Last update 12 March 2001.
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© Mark Wade, 2001 .