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- NK-33 abstract "The NK-33 and NK-43 are rocket engines designed and built in the late 1960s and early 1970s by the Kuznetsov Design Bureau. The NK designation is presumably derived from the name of the chief designer, Nikolay Kuznetsov. They were intended for the ill-fated Soviet N-1 rocket moon shot. The NK-33 engine is among the highest thrust-to-weight ratio of any Earth-launchable rocket engine (second only to SpaceX Merlin 1D engine), while achieving a very high specific impulse. NK-33 was by many measures the highest performance LOX/kerosene rocket engine ever created.The NK-43 is similar to the NK-33, but is designed for an upper stage, not a first stage. It has a longer nozzle, optimized for operation at altitude, where ambient air pressure is low or perhaps zero. This gives it a higher thrust and specific impulse, but makes it longer and heavier.Modified versions of these engines by Aerojet are known as the AJ26-58, AJ26-59 and AJ26-62.In 2010 stockpiled NK-33 engines were successfully tested for use by the Orbital Sciences Antares light-to-medium-lift launcher.".
- NK-33 thumbnail Aerojet_AJ26_in_the_Stennis_E-1_Test_Stand_-_cropped.jpg?width=300.
- NK-33 wikiPageExternalLink index.htm.
- NK-33 wikiPageExternalLink nk33_specs.shtml.
- NK-33 wikiPageExternalLink watch?v=MZnYr94aa9E.
- NK-33 wikiPageID "3813298".
- NK-33 wikiPageRevisionID "602050129".
- NK-33 caption "The Russian NK-33 was modified and renamed the AJ26-58 by Aerojet. This AJ26-58 is shown during a test firing at Stennis Space Center".
- NK-33 countryOfOrigin Soviet_Union.
- NK-33 cycle Staged_combustion_cycle.
- NK-33 date "1970.0".
- NK-33 designer Kuznetsov_Design_Bureau.
- NK-33 fuel RP-1.
- NK-33 hasPhotoCollection NK-33.
- NK-33 imsize "200".
- NK-33 name "NK-33".
- NK-33 oxidiser Liquid_oxygen.
- NK-33 predecessor "NK-15, NK-15V".
- NK-33 pumps Turbopump.
- NK-33 purpose "1".
- NK-33 successor "AJ26-58, AJ26-59, AJ26-62".
- NK-33 thrustToWeight "137".
- NK-33 type "liquid".
- NK-33 subject Category:Kerosene_rocket_engines.
- NK-33 subject Category:Rocket_engines.
- NK-33 subject Category:Rocket_engines_of_the_Soviet_Union.
- NK-33 subject Category:Science_and_technology_in_the_Soviet_Union.
- NK-33 subject Category:Soviet_lunar_program.
- NK-33 comment "The NK-33 and NK-43 are rocket engines designed and built in the late 1960s and early 1970s by the Kuznetsov Design Bureau. The NK designation is presumably derived from the name of the chief designer, Nikolay Kuznetsov. They were intended for the ill-fated Soviet N-1 rocket moon shot. The NK-33 engine is among the highest thrust-to-weight ratio of any Earth-launchable rocket engine (second only to SpaceX Merlin 1D engine), while achieving a very high specific impulse.".
- NK-33 label "Kusnezow NK-33".
- NK-33 label "NK-33".
- NK-33 label "NK-33".
- NK-33 label "NK-33".
- NK-33 label "NK-33".
- NK-33 label "NK-33".
- NK-33 label "NK-33火箭发动机".
- NK-33 label "НК-33".
- NK-33 sameAs Kusnezow_NK-33.
- NK-33 sameAs NK-33.
- NK-33 sameAs NK-33.
- NK-33 sameAs NK-33.
- NK-33 sameAs NK-33.
- NK-33 sameAs NK-33.
- NK-33 sameAs NK-33.
- NK-33 sameAs m.0b19_q.
- NK-33 sameAs Q1516025.
- NK-33 sameAs Q1516025.
- NK-33 wasDerivedFrom NK-33?oldid=602050129.
- NK-33 depiction Aerojet_AJ26_in_the_Stennis_E-1_Test_Stand_-_cropped.jpg.
- NK-33 isPrimaryTopicOf NK-33.
