Plug-Nozzle SASSTO

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Engine Model: Plug-Nozzle SASSTO. Propellants: Lox/LH2. Thrust(vac): 1,574.900 kN (354,052 lbf). Thrust(sl): 1,231.800 kN (276,920 lbf). Isp: 459 sec. Isp (sea level): 359 sec. Burn time: 268 sec. Chambers: 1. Country: USA. Status: Study 1967. Plug-Nozzle SASSTO used on Rocket Stages Used on stage: SASSTO. on launch vehicle: SASSTO. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.