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RS-18

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z RS-18 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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z © 1997-2019 Mark Wade - Contact © / Conditions for Use

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