This page no longer updated from 31 October 2001. Latest version can be found at SSME Study

Used on stages: Shuttle DC-3-1, Shuttle DC-3-2, Shuttle FR-3-1, Shuttle FR-3-2, Shuttle H33-1, Shuttle H33-2, Shuttle HCR-1, Shuttle HCR-2, Shuttle LCR-1, Shuttle LCR-2, Shuttle LS A-1, Shuttle LS A-2, Shuttle LS200-1, Shuttle MDC-A-1, Shuttle MDC-A-2, Shuttle NAR A-1, S. Used on launch vehicles: Shuttle DC-3, Shuttle FR-3, Shuttle H33, Shuttle HCR, Shuttle LCR, Shuttle LS A, Shuttle LS200, Shuttle MDC, Shuttle NAR A, Shuttle R134C, Spacemaster. Propellants: Lox/LH2 Thrust(vac): 156,550 kgf. Thrust(vac): 1,535.20 kN. Isp: 459 sec. Isp (sea level): 359 sec. Burn time: 379 sec. Chambers: 1. Country: USA. Status: Study 1970.
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Last update 12 March 2001.
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© Mark Wade, 2001 .