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- Delta-P abstract "The Delta-P is an American rocket stage, developed by McDonnell Douglas and TRW, first used on November 10, 1972 as the second stage for the Delta 1000 series.It continued to serve as the second stage for subsequent Delta 2000 and Delta 3000 flights for 17 years, with its last usage on March 24, 1989.It is propelled by a single TRW TR-201 rocket engine, fueled by Aerozine 50 and dinitrogen tetroxide, which are hypergolic.The Delta-P traces its heritage to the Apollo Lunar Module's Descent Propulsion System. The TR-201 engine is the Descent Propulsion System modified to be a fixed thrust engine. The Descent Propulsion System was first fired in flight during the Apollo 5 mission, in a low Earth orbit test on January 22, 1968.As the supply of these surplus Apollo engines was depleted, the Douglas/Aerojet Delta-K upper stage was introduced in the Delta 3000 program. The Delta-K was then exclusively used on the second stage for the Delta 4000, Delta 5000, and subsequent Delta II.".
- Delta-P wikiPageID "39956828".
- Delta-P wikiPageLength "2268".
- Delta-P wikiPageOutDegree "30".
- Delta-P wikiPageRevisionID "654464568".
- Delta-P wikiPageWikiLink Aerozine_50.
- Delta-P wikiPageWikiLink Apollo_5.
- Delta-P wikiPageWikiLink Apollo_Lunar_Module.
- Delta-P wikiPageWikiLink Apollo_program.
- Delta-P wikiPageWikiLink Category:Rocket_stages.
- Delta-P wikiPageWikiLink Delta-K.
- Delta-P wikiPageWikiLink Delta_1000.
- Delta-P wikiPageWikiLink Delta_2000.
- Delta-P wikiPageWikiLink Delta_3000.
- Delta-P wikiPageWikiLink Delta_4000.
- Delta-P wikiPageWikiLink Delta_5000.
- Delta-P wikiPageWikiLink Delta_II.
- Delta-P wikiPageWikiLink Descent_Propulsion_System.
- Delta-P wikiPageWikiLink Dinitrogen_tetroxide.
- Delta-P wikiPageWikiLink Hypergolic.
- Delta-P wikiPageWikiLink Hypergolic_propellant.
- Delta-P wikiPageWikiLink Low_Earth_orbit.
- Delta-P wikiPageWikiLink McDonnell_Douglas.
- Delta-P wikiPageWikiLink Multistage_rocket.
- Delta-P wikiPageWikiLink N2O4.
- Delta-P wikiPageWikiLink Rocket.
- Delta-P wikiPageWikiLink TR-201.
- Delta-P wikiPageWikiLink TRW_Inc..
- Delta-P wikiPageWikiLink USA.
- Delta-P wikiPageWikiLink United_States.
- Delta-P wikiPageWikiLink Upper_stage.
- Delta-P wikiPageWikiLinkText "Delta-P".
- Delta-P countryOrigin USA.
- Delta-P countryOrigin United_States.
- Delta-P engines "1".
- Delta-P fuel Aerozine_50.
- Delta-P fuel Dinitrogen_tetroxide.
- Delta-P fuel N2O4.
- Delta-P hasPhotoCollection Delta-P.
- Delta-P manufacturer "TRW and McDonnell Douglas".
- Delta-P rockets Delta_1000.
- Delta-P rockets Delta_2000.
- Delta-P rockets Delta_3000.
- Delta-P si "319.0".
- Delta-P time "431.0".
- Delta-P wikiPageUsesTemplate Template:Infobox_rocket_stage.
- Delta-P wikiPageUsesTemplate Template:Reflist.
- Delta-P wikiPageUsesTemplate Template:Rocket-stub.
- Delta-P wikiPageUsesTemplate Template:Upper_stages.
- Delta-P subject Category:Rocket_stages.
- Delta-P hypernym Stage.
- Delta-P type Person.
- Delta-P comment "The Delta-P is an American rocket stage, developed by McDonnell Douglas and TRW, first used on November 10, 1972 as the second stage for the Delta 1000 series.It continued to serve as the second stage for subsequent Delta 2000 and Delta 3000 flights for 17 years, with its last usage on March 24, 1989.It is propelled by a single TRW TR-201 rocket engine, fueled by Aerozine 50 and dinitrogen tetroxide, which are hypergolic.The Delta-P traces its heritage to the Apollo Lunar Module's Descent Propulsion System. ".
- Delta-P label "Delta-P".
- Delta-P sameAs Delta_P.
- Delta-P sameAs Delta_P.
- Delta-P sameAs m.0wbnfp5.
- Delta-P sameAs Q49556.
- Delta-P sameAs Q49556.
- Delta-P wasDerivedFrom Delta-P?oldid=654464568.
- Delta-P isPrimaryTopicOf Delta-P.