Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Descent_Propulsion_System> ?p ?o }
- 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 wikiPageLength "10863".
- Descent_Propulsion_System wikiPageOutDegree "50".
- Descent_Propulsion_System wikiPageRevisionID "673320540".
- Descent_Propulsion_System wikiPageWikiLink AS-201.
- Descent_Propulsion_System wikiPageWikiLink Aerojet.
- Descent_Propulsion_System wikiPageWikiLink Aerozine_50.
- Descent_Propulsion_System wikiPageWikiLink Apollo_13.
- Descent_Propulsion_System wikiPageWikiLink Apollo_15.
- Descent_Propulsion_System wikiPageWikiLink Service_Module.
- Descent_Propulsion_System wikiPageWikiLink Apollo_Lunar_Module.
- Descent_Propulsion_System wikiPageWikiLink Apollo_Service_Module.
- Descent_Propulsion_System wikiPageWikiLink Atlantic_Ocean.
- Descent_Propulsion_System wikiPageWikiLink Category:Apollo_program_hardware.
- Descent_Propulsion_System wikiPageWikiLink Category:Rocket_engines.
- Descent_Propulsion_System wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- Descent_Propulsion_System wikiPageWikiLink Category:TRW_Inc..
- Descent_Propulsion_System wikiPageWikiLink Delta-P.
- Descent_Propulsion_System wikiPageWikiLink Delta_1000.
- Descent_Propulsion_System wikiPageWikiLink Delta_2000.
- Descent_Propulsion_System wikiPageWikiLink Delta_3000.
- Descent_Propulsion_System wikiPageWikiLink Dinitrogen_tetroxide.
- Descent_Propulsion_System wikiPageWikiLink Free_return_trajectory.
- Descent_Propulsion_System wikiPageWikiLink Gimbaled_thrust.
- Descent_Propulsion_System wikiPageWikiLink Gimballed_thrust.
- Descent_Propulsion_System wikiPageWikiLink Helium.
- Descent_Propulsion_System wikiPageWikiLink Hypergolic.
- Descent_Propulsion_System wikiPageWikiLink Hypergolic_propellant.
- Descent_Propulsion_System wikiPageWikiLink Joseph_Francis_Shea.
- Descent_Propulsion_System wikiPageWikiLink Lunar_Module.
- Descent_Propulsion_System wikiPageWikiLink Lunar_orbit.
- Descent_Propulsion_System wikiPageWikiLink Lyndon_B._Johnson_Space_Center.
- Descent_Propulsion_System wikiPageWikiLink Maxime_Faget.
- Descent_Propulsion_System wikiPageWikiLink Merlin_(rocket_engine).
- Descent_Propulsion_System wikiPageWikiLink Merlin_(rocket_engine_family).
- Descent_Propulsion_System wikiPageWikiLink N2O4.
- Descent_Propulsion_System wikiPageWikiLink Pericynthion.
- Descent_Propulsion_System wikiPageWikiLink Pintle_injector.
- Descent_Propulsion_System wikiPageWikiLink Pressure-fed_engine.
- Descent_Propulsion_System wikiPageWikiLink Pressure-fed_engine_(rocket).
- Descent_Propulsion_System wikiPageWikiLink Robert_R._Gilruth.
- Descent_Propulsion_System wikiPageWikiLink Rocket_engine.
- Descent_Propulsion_System wikiPageWikiLink Rocketdyne.
- Descent_Propulsion_System wikiPageWikiLink Service_Propulsion_System.
- Descent_Propulsion_System wikiPageWikiLink Spacecraft.
- Descent_Propulsion_System wikiPageWikiLink TR-201.
- Descent_Propulsion_System wikiPageWikiLink TRW_Inc..
- Descent_Propulsion_System wikiPageWikiLink Thiokol.
- Descent_Propulsion_System wikiPageWikiLink Throttle.
- Descent_Propulsion_System wikiPageWikiLink Turbopump.
- Descent_Propulsion_System wikiPageWikiLink US_Navy.
- Descent_Propulsion_System wikiPageWikiLink United_Aircraft.
- Descent_Propulsion_System wikiPageWikiLink United_States_Navy.
- Descent_Propulsion_System wikiPageWikiLink File:Apollo_15_Engine_Bell.jpg.
- Descent_Propulsion_System wikiPageWikiLinkText "Descent Propulsion System".
- Descent_Propulsion_System wikiPageWikiLinkText "LM Descent Engine (LMDE)".
- Descent_Propulsion_System wikiPageWikiLinkText "LMDE".
- Descent_Propulsion_System wikiPageWikiLinkText "Lunar Module Descent Engine (LMDE)".
- Descent_Propulsion_System wikiPageWikiLinkText "Lunar Module Descent Engine [LMDE] (Apollo program)".
- Descent_Propulsion_System wikiPageWikiLinkText "Lunar Module Descent Engine".
- Descent_Propulsion_System wikiPageWikiLinkText "descent engine or (LMDE)".
- Descent_Propulsion_System wikiPageWikiLinkText "descent engine".
- Descent_Propulsion_System wikiPageWikiLinkText "descent rocket engine".
- Descent_Propulsion_System wikiPageWikiLinkText "descent stage engine".
- Descent_Propulsion_System chamberPressure "100".
- Descent_Propulsion_System combustionChamber "1".
- Descent_Propulsion_System cycle Pressure-fed_engine.
- Descent_Propulsion_System cycle Pressure-fed_engine_(rocket).
- 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 oxidizer N2O4.
- 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 wikiPageUsesTemplate Template:Apollo_program_hardware.
- Descent_Propulsion_System wikiPageUsesTemplate Template:Convert.
- Descent_Propulsion_System wikiPageUsesTemplate Template:Infobox_rocket_engine.
- Descent_Propulsion_System wikiPageUsesTemplate Template:Orbital_spacecraft_rocket_engines.
- Descent_Propulsion_System wikiPageUsesTemplate Template:Reflist.
- Descent_Propulsion_System wikiPageUsesTemplate Template:TRW.
- Descent_Propulsion_System subject Category:Apollo_program_hardware.
- Descent_Propulsion_System subject Category:Rocket_engines.
- Descent_Propulsion_System subject Category:Rocket_engines_using_hypergolic_propellant.
- Descent_Propulsion_System subject Category:TRW_Inc..
- Descent_Propulsion_System hypernym Engine.
- Descent_Propulsion_System type Software.
- 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.