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- Delta-K abstract "The Delta-K is an American rocket stage, developed by McDonnell Douglas and Aerojet. It was first used on August 27, 1989 as the second stage for the Delta 4000 series.It has continued to serve as the second stage for subsequent variants of the Delta rocket.It is propelled by a single AJ10-118K rocket engine, fueled by Aerozine 50 and dinitrogen tetroxide, which are hypergolic.The Delta-K has a long heritage to the first Able stage used in Project Vanguard. The AJ-10 engine was first used in the Able second stage of the Vanguard rocket, as the AJ10-118 configuration. It was initially fueled by nitric acid and UDMH. An AJ10 engine was first fired in flight during the third Vanguard launch, on 17 March 1958, which successfully placed the Vanguard 1 satellite into orbit.As of 25 May 2008, 138 have been launched, and excluding one which was destroyed by the explosion of a lower stage, none have failed.The Delta-K is still in use, currently as the second stage of the Delta II rocket.".
- Delta-K thumbnail Delta-II_Stage2_XSS-10.jpg?width=300.
- Delta-K wikiPageID "17602697".
- Delta-K wikiPageLength "2978".
- Delta-K wikiPageOutDegree "31".
- Delta-K wikiPageRevisionID "649808235".
- Delta-K wikiPageWikiLink AJ10.
- Delta-K wikiPageWikiLink Able_(rocket_stage).
- Delta-K wikiPageWikiLink Advanced_Cryogenic_Evolved_Stage.
- Delta-K wikiPageWikiLink Aerozine_50.
- Delta-K wikiPageWikiLink Boeing.
- Delta-K wikiPageWikiLink Category:Rocket_stages.
- Delta-K wikiPageWikiLink Delta_(rocket_family).
- Delta-K wikiPageWikiLink Delta_4000.
- Delta-K wikiPageWikiLink Delta_5000.
- Delta-K wikiPageWikiLink Delta_Cryogenic_Second_Stage.
- Delta-K wikiPageWikiLink Delta_II.
- Delta-K wikiPageWikiLink Dinitrogen_tetroxide.
- Delta-K wikiPageWikiLink Hypergolic_propellant.
- Delta-K wikiPageWikiLink McDonnell_Douglas.
- Delta-K wikiPageWikiLink Multistage_rocket.
- Delta-K wikiPageWikiLink Nitric_acid.
- Delta-K wikiPageWikiLink Rocket.
- Delta-K wikiPageWikiLink Transtage.
- Delta-K wikiPageWikiLink United_Launch_Alliance.
- Delta-K wikiPageWikiLink United_States.
- Delta-K wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- Delta-K wikiPageWikiLink Vanguard_(rocket).
- Delta-K wikiPageWikiLink Vanguard_1.
- Delta-K wikiPageWikiLink File:Delta-II_Stage2_XSS-10.jpg.
- Delta-K wikiPageWikiLinkText "Delta-K".
- Delta-K countryOrigin United_States.
- Delta-K engines "1".
- Delta-K fuel Aerozine_50.
- Delta-K fuel Dinitrogen_tetroxide.
- Delta-K manufacturer United_Launch_Alliance.
- Delta-K rockets Delta_4000.
- Delta-K rockets Delta_5000.
- Delta-K rockets Delta_II.
- Delta-K si "319.0".
- Delta-K time "431.0".
- Delta-K wikiPageUsesTemplate Template:Convert.
- Delta-K wikiPageUsesTemplate Template:Infobox_rocket_stage.
- Delta-K wikiPageUsesTemplate Template:Reflist.
- Delta-K wikiPageUsesTemplate Template:Rocket-stub.
- Delta-K wikiPageUsesTemplate Template:Upper_stages.
- Delta-K wikiPageUsesTemplate Template:Use_dmy_dates.
- Delta-K subject Category:Rocket_stages.
- Delta-K hypernym Stage.
- Delta-K type Person.
- Delta-K type Stage.
- Delta-K comment "The Delta-K is an American rocket stage, developed by McDonnell Douglas and Aerojet. It was first used on August 27, 1989 as the second stage for the Delta 4000 series.It has continued to serve as the second stage for subsequent variants of the Delta rocket.It is propelled by a single AJ10-118K rocket engine, fueled by Aerozine 50 and dinitrogen tetroxide, which are hypergolic.The Delta-K has a long heritage to the first Able stage used in Project Vanguard.".
- Delta-K label "Delta-K".
- Delta-K sameAs Q49548.
- Delta-K sameAs Делта-К.
- Delta-K sameAs Delta_K.
- Delta-K sameAs Delta-K.
- Delta-K sameAs Delta-K.
- Delta-K sameAs Delta_K.
- Delta-K sameAs m.0464jz4.
- Delta-K sameAs Q49548.
- Delta-K wasDerivedFrom Delta-K?oldid=649808235.
- Delta-K depiction Delta-II_Stage2_XSS-10.jpg.
- Delta-K isPrimaryTopicOf Delta-K.