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- Descent_Propulsion_System abstract "The Descent Propulsion System (DPS) or LMDE (Lunar Module Descent Engine) is a variable throttle hypergolic rocket engine developed by Space Technology Laboratories (TRW) for use in the Apollo Lunar Module Descent Stage. It used Aerozine 50 fuel and N2O4 oxidizer. This engine used a pintle injector, a design also used later in the SpaceX Merlin engine.".
- Descent_Propulsion_System wikiPageExternalLink 19730011150_1973011150.pdf.
- Descent_Propulsion_System wikiPageExternalLink 20090016298_2009014419.pdf.
- Descent_Propulsion_System wikiPageExternalLink donharvey1.htm.
- Descent_Propulsion_System wikiPageID "35997160".
- Descent_Propulsion_System wikiPageRevisionID "599314994".
- Descent_Propulsion_System chamberPressure "100".
- Descent_Propulsion_System combustionChamber "1".
- Descent_Propulsion_System cycle Pressure-fed_engine.
- Descent_Propulsion_System date "1964".
- Descent_Propulsion_System fuel Aerozine_50.
- Descent_Propulsion_System hasPhotoCollection Descent_Propulsion_System.
- Descent_Propulsion_System manufacturer TRW_Inc..
- Descent_Propulsion_System name "Descent Propulsion System".
- Descent_Propulsion_System oxidizer Dinitrogen_tetroxide.
- Descent_Propulsion_System purpose "Lunar Descent Stage/Spacecraft propulsion".
- Descent_Propulsion_System status "Retired".
- Descent_Propulsion_System successor TR-201.
- Descent_Propulsion_System thrust(vac)_ "maximum, throttle between 10% and 60% of full thrust".
- Descent_Propulsion_System type "liquid".
- Descent_Propulsion_System usedIn "Lunar Module as Descent Engine".
- Descent_Propulsion_System subject Category:Apollo_program_hardware.
- Descent_Propulsion_System subject Category:Rocket_engines.
- Descent_Propulsion_System comment "The Descent Propulsion System (DPS) or LMDE (Lunar Module Descent Engine) is a variable throttle hypergolic rocket engine developed by Space Technology Laboratories (TRW) for use in the Apollo Lunar Module Descent Stage. It used Aerozine 50 fuel and N2O4 oxidizer. This engine used a pintle injector, a design also used later in the SpaceX Merlin engine.".
- Descent_Propulsion_System label "Descent Propulsion System".
- Descent_Propulsion_System sameAs Descent_Propulsion_System.
- Descent_Propulsion_System sameAs m.0j_7163.
- Descent_Propulsion_System sameAs Q5263733.
- Descent_Propulsion_System sameAs Q5263733.
- Descent_Propulsion_System wasDerivedFrom Descent_Propulsion_System?oldid=599314994.
- Descent_Propulsion_System isPrimaryTopicOf Descent_Propulsion_System.