SSME Study
Propellants: Lox/LH2. Thrust(vac): 1,535.200 kN (345,127 lbf). Thrust(sl): 1,200.700 kN (269,928 lbf). Isp: 459 sec. Isp (sea level): 359 sec. Burn time: 379 sec. Chambers: 1. Country: USA. Status: Study 1967.


SSME Study used on Rocket Stages

 
 
 
 
 
 
 
 
 

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