AKA: RS-30. Date: 1970. Thrust: 88.93 kN (19,991 lbf). Specific impulse: 473 s.
Subtopics 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. Country: USA. Spacecraft: LEV. Propellants: Lox/LH2. Agency: Rocketdyne. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9RetroSearch is an open source project built by @garambo | Open a GitHub Issue
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