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RS-18
RS-18 / LMDE
RS-18 / LMDE
Credit: Boeing / Rocketdyne
Rocketdyne N2O4/Aerozine-50 rocket engine. Apollo Lunar Ascent Module Engine. Pressure-fed.

Date: 1967. Thrust: 15.56 kN (3,499 lbf). Specific impulse: 310 s.



Subtopics

RS-34 Rocketdyne N2O4/MMH rocket engine. Peacekeeper Postboost Axial Thrust. Pressure-fed. 1 main axial thruster per postboost propulsion system. First flight 1983.

RS-41 Rocketdyne N2O4/MMH rocket engine. Axial Spacecraft. Pressure-fed.

XLR132 Rocketdyne N2O4/MMH rocket engine. Out of Production. Pump-fed high performance upper stage engine for perigee/apogee stages. as well as transfer vehicles and lunar and Martian missions. Tested extensively but no production.

RS-51 Rocketdyne N2O4/MMH rocket engine. Axial Spacecraft. Pressure-fed.

Family: Storable liquid. Country: USA. Propellants: N2O4/Aerozine-50. Agency: Rocketdyne.

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