ASE Credit: Boeing / Rocketdyne |
AKA: RS-30. Date: 1970. Thrust: 88.93 kN (19,991 lbf). Specific impulse: 473 s.
AMPS-1 Rocketdyne LOx/LH2 rocket engine. Advanced Maneuvering Propulsion System Booster. Pressure-fed. |
AEC engine Rocketdyne LOx/LH2 rocket engine. Advanced Expander Cycle Engine. Expander regenerator, pump-fed. |