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- HG-3_(rocket_engine) abstract "The HG-3 was a liquid-fuel cryogenic rocket engine which was designed for use on the upper stages of Saturn rockets in the post-Apollo era. Designed in the United States by Rocketdyne, the HG-3 would have burned cryogenic liquid hydrogen & liquid oxygen propellants, with each engine producing 1,400.7 kN (315,000 lbf) of thrust during flight. The engine was designed to produce a specific impulse (Isp) of 451 seconds in a vacuum, or 280 seconds at sea level. Developed from Rocketdyne's J-2 engine used on the S-II and S-IVB stages, the engine was intended to replace the J-2 on the upgraded S-II-2 and S-IVB-2 stages intended for use on the Saturn MLV, Saturn IB-B and Saturn V/4-260 rockets, with a sea-level optimised version, the HG-3-SL, intended for use on the Saturn INT-17. The engine was cancelled, however, during the post-Apollo drawdown when development of the more advanced Saturn rockets ceased, and never flew, although the engine was later used as the basis for the design of the RS-25 Space Shuttle Main Engine.".
- HG-3_(rocket_engine) wikiPageID "34785687".
- HG-3_(rocket_engine) wikiPageLength "3499".
- HG-3_(rocket_engine) wikiPageOutDegree "38".
- HG-3_(rocket_engine) wikiPageRevisionID "699953249".
- HG-3_(rocket_engine) wikiPageWikiLink Apollo_program.
- HG-3_(rocket_engine) wikiPageWikiLink Category:Rocket_engines_using_hydrogen_propellant.
- HG-3_(rocket_engine) wikiPageWikiLink Category:Rocketdyne_engines.
- HG-3_(rocket_engine) wikiPageWikiLink Cryogenic_fuel.
- HG-3_(rocket_engine) wikiPageWikiLink Cryogenic_rocket_engine.
- HG-3_(rocket_engine) wikiPageWikiLink J-2X.
- HG-3_(rocket_engine) wikiPageWikiLink Liquid-propellant_rocket.
- HG-3_(rocket_engine) wikiPageWikiLink Liquid_hydrogen.
- HG-3_(rocket_engine) wikiPageWikiLink Liquid_oxygen.
- HG-3_(rocket_engine) wikiPageWikiLink Marshall_Space_Flight_Center.
- HG-3_(rocket_engine) wikiPageWikiLink Multistage_rocket.
- HG-3_(rocket_engine) wikiPageWikiLink Rocketdyne.
- HG-3_(rocket_engine) wikiPageWikiLink Rocketdyne_J-2.
- HG-3_(rocket_engine) wikiPageWikiLink S-II.
- HG-3_(rocket_engine) wikiPageWikiLink S-II-2.
- HG-3_(rocket_engine) wikiPageWikiLink S-IVB.
- HG-3_(rocket_engine) wikiPageWikiLink S-IVB-2.
- HG-3_(rocket_engine) wikiPageWikiLink Saturn_(rocket_family).
- HG-3_(rocket_engine) wikiPageWikiLink Saturn_IB-B.
- HG-3_(rocket_engine) wikiPageWikiLink Saturn_II.
- HG-3_(rocket_engine) wikiPageWikiLink Saturn_MLV.
- HG-3_(rocket_engine) wikiPageWikiLink 4-260.
- HG-3_(rocket_engine) wikiPageWikiLink Space_Shuttle_main_engine.
- HG-3_(rocket_engine) wikiPageWikiLink Specific_impulse.
- HG-3_(rocket_engine) wikiPageWikiLink Thrust.
- HG-3_(rocket_engine) wikiPageWikiLink United_States.
- HG-3_(rocket_engine) wikiPageWikiLinkText "HG-3 (rocket engine)".
- HG-3_(rocket_engine) wikiPageWikiLinkText "HG-3 engine".
- HG-3_(rocket_engine) wikiPageWikiLinkText "HG-3 engines".
- HG-3_(rocket_engine) wikiPageWikiLinkText "HG-3".
- HG-3_(rocket_engine) wikiPageWikiLinkText "HG-3-SL".
- HG-3_(rocket_engine) wikiPageWikiLinkText "Rocketdyne HG-3".
- HG-3_(rocket_engine) associated Saturn_IB-B.
- HG-3_(rocket_engine) associated Saturn_II.
- HG-3_(rocket_engine) associated Saturn_MLV.
- HG-3_(rocket_engine) associated 4-260.
- HG-3_(rocket_engine) countryOfOrigin United_States.
- HG-3_(rocket_engine) designer Marshall_Space_Flight_Center.
- HG-3_(rocket_engine) designer Rocketdyne.
- HG-3_(rocket_engine) fuel Liquid_hydrogen.
- HG-3_(rocket_engine) manufacturer Rocketdyne.
- HG-3_(rocket_engine) name "HG-3".
- HG-3_(rocket_engine) oxidiser Liquid_oxygen.
- HG-3_(rocket_engine) predecessor Rocketdyne_J-2.
- HG-3_(rocket_engine) purpose "Upper stage engine".
- HG-3_(rocket_engine) status "Cancelled during development.".
- HG-3_(rocket_engine) successor Space_Shuttle_main_engine.
- HG-3_(rocket_engine) type "liquid".
- HG-3_(rocket_engine) wikiPageUsesTemplate Template:Convert.
- HG-3_(rocket_engine) wikiPageUsesTemplate Template:Infobox_rocket_engine.
- HG-3_(rocket_engine) wikiPageUsesTemplate Template:Reflist.
- HG-3_(rocket_engine) wikiPageUsesTemplate Template:Rocketry-stub.
- HG-3_(rocket_engine) subject Category:Rocket_engines_using_hydrogen_propellant.
- HG-3_(rocket_engine) subject Category:Rocketdyne_engines.
- HG-3_(rocket_engine) hypernym Engine.
- HG-3_(rocket_engine) type Company.
- HG-3_(rocket_engine) type Software.
- HG-3_(rocket_engine) type Company.
- HG-3_(rocket_engine) type Technology.
- HG-3_(rocket_engine) comment "The HG-3 was a liquid-fuel cryogenic rocket engine which was designed for use on the upper stages of Saturn rockets in the post-Apollo era. Designed in the United States by Rocketdyne, the HG-3 would have burned cryogenic liquid hydrogen & liquid oxygen propellants, with each engine producing 1,400.7 kN (315,000 lbf) of thrust during flight. The engine was designed to produce a specific impulse (Isp) of 451 seconds in a vacuum, or 280 seconds at sea level.".
- HG-3_(rocket_engine) label "HG-3 (rocket engine)".
- HG-3_(rocket_engine) sameAs Q5629533.
- HG-3_(rocket_engine) sameAs HG-3_(ロケットエンジン).
- HG-3_(rocket_engine) sameAs m.0j3c7dj.
- HG-3_(rocket_engine) sameAs Q5629533.
- HG-3_(rocket_engine) wasDerivedFrom HG-3_(rocket_engine)?oldid=699953249.
- HG-3_(rocket_engine) isPrimaryTopicOf HG-3_(rocket_engine).