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RS-76
RS-76
RS-76
Credit: Boeing / Rocketdyne
Rocketdyne LOx/Kerosene rocket engine. Space Shuttle Reusable First Stage. Ox-Rich staged combustion, pump-fed. Thrust and specific impulse values are at sea level.

Date: 1998. Thrust: 4,002.00 kN (899,685 lbf). Specific impulse: 308 s. Specific impulse sea level: 308 s.

Thrust (sl): 4,002.000 kN (899,685 lbf). Thrust (sl): 408,100 kgf. Propellant Formulation: Lox/RP-1 or JP-8.



Country: USA. Propellants: Lox/Kerosene. Agency: Rocketdyne.

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