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- LE-7 abstract "The LE-7 and its succeeding upgrade model the LE-7A are staged combustion cycle LH2/LOX liquid rocket engines produced in Japan for the H-II series of launch vehicles. Design and production work was all done domestically in Japan, the first major (main/first-stage) liquid rocket engine with that claim, in a collaborative effort from the National Space Development Agency (NASDA), Aerospace Engineering Laboratory (NAL), Mitsubishi Heavy Industries, and Ishikawajima-Harima. NASDA and NAL have since been integrated into JAXA. However, a large part of the work was contracted to Mitsubishi, with Ishikawajima-Harima providing turbomachinery, and the engine is often referred to as the Mitsubishi LE-7(A).The original LE-7 was designed to be a high efficiency, medium-sized motor with sufficient thrust for use on the H-II, and classified as expendable since the engine was non-recoverable after launch.".
- LE-7 thumbnail LE-7_rocket_engine.jpg?width=300.
- LE-7 wikiPageExternalLink le7.htm.
- LE-7 wikiPageExternalLink le7a.htm.
- LE-7 wikiPageExternalLink h-2af8.pdf.
- LE-7 wikiPageExternalLink e392051.pdf.
- LE-7 wikiPageID "15496163".
- LE-7 wikiPageLength "7429".
- LE-7 wikiPageOutDegree "49".
- LE-7 wikiPageRevisionID "699951174".
- LE-7 wikiPageWikiLink Actuator.
- LE-7 wikiPageWikiLink Axial-flow_pump.
- LE-7 wikiPageWikiLink Booster_(rocketry).
- LE-7 wikiPageWikiLink Casting.
- LE-7 wikiPageWikiLink Category:Rocket_engines.
- LE-7 wikiPageWikiLink Category:Rocket_engines_of_Japan.
- LE-7 wikiPageWikiLink Category:Rocket_engines_using_hydrogen_propellant.
- LE-7 wikiPageWikiLink Cavitation.
- LE-7 wikiPageWikiLink Comparison_of_orbital_rocket_engines.
- LE-7 wikiPageWikiLink Computational_fluid_dynamics.
- LE-7 wikiPageWikiLink Expendable_launch_system.
- LE-7 wikiPageWikiLink Fatigue_(material).
- LE-7 wikiPageWikiLink Gimbal.
- LE-7 wikiPageWikiLink H-II.
- LE-7 wikiPageWikiLink H-IIA.
- LE-7 wikiPageWikiLink H-IIB.
- LE-7 wikiPageWikiLink IHI_Corporation.
- LE-7 wikiPageWikiLink JAXA.
- LE-7 wikiPageWikiLink Japan.
- LE-7 wikiPageWikiLink LE-5.
- LE-7 wikiPageWikiLink Liquid-propellant_rocket.
- LE-7 wikiPageWikiLink Liquid_hydrogen.
- LE-7 wikiPageWikiLink Liquid_oxygen.
- LE-7 wikiPageWikiLink Machining.
- LE-7 wikiPageWikiLink Mitsubishi_Heavy_Industries.
- LE-7 wikiPageWikiLink Multistage_rocket.
- LE-7 wikiPageWikiLink Nozzle.
- LE-7 wikiPageWikiLink Propellant.
- LE-7 wikiPageWikiLink Regenerative_cooling_(rocket).
- LE-7 wikiPageWikiLink Staged_combustion_cycle.
- LE-7 wikiPageWikiLink Turbomachinery.
- LE-7 wikiPageWikiLink Turbopump.
- LE-7 wikiPageWikiLink Vibration.
- LE-7 wikiPageWikiLink Welding.
- LE-7 wikiPageWikiLink File:Mitsubishi_LE-7A.JPG.
- LE-7 wikiPageWikiLinkText "LE-7 / 7A".
- LE-7 wikiPageWikiLinkText "LE-7".
- LE-7 wikiPageWikiLinkText "LE-7#LE-7A".
- LE-7 wikiPageWikiLinkText "LE-7/7A".
- LE-7 wikiPageWikiLinkText "LE-7A".
- LE-7 caption "LE-7, Nagoya City Science Museum, 2006".
- LE-7 combustionChamber "1".
- LE-7 countryOfOrigin Japan.
- LE-7 cycle Staged_combustion_cycle.
- LE-7 designer JAXA.
- LE-7 fuel Liquid_hydrogen.
- LE-7 imageSize "250".
- LE-7 length "3.4 m".
- LE-7 manufacturer Mitsubishi_Heavy_Industries.
- LE-7 mixture "5.9".
- LE-7 name "LE-7".
- LE-7 nozzleRatio "52".
- LE-7 oxidiser Liquid_oxygen.
- LE-7 purpose Booster_(rocketry).
- LE-7 status "Succeeded by LE-7A upgrade".
- LE-7 thrustToWeight "64.13".
- LE-7 type "liquid".
- LE-7 usedIn "H-II first stage".
- LE-7 wikiPageUsesTemplate Template:Commons_category.
- LE-7 wikiPageUsesTemplate Template:Convert.
- LE-7 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- LE-7 wikiPageUsesTemplate Template:Reflist.
- LE-7 wikiPageUsesTemplate Template:Rocket_Engines.
- LE-7 subject Category:Rocket_engines.
- LE-7 subject Category:Rocket_engines_of_Japan.
- LE-7 subject Category:Rocket_engines_using_hydrogen_propellant.
- LE-7 hypernym http://dbpedia.org/resource//.
- LE-7 type Program.
- LE-7 type Redirect.
- LE-7 type Technology.
- LE-7 comment "The LE-7 and its succeeding upgrade model the LE-7A are staged combustion cycle LH2/LOX liquid rocket engines produced in Japan for the H-II series of launch vehicles. Design and production work was all done domestically in Japan, the first major (main/first-stage) liquid rocket engine with that claim, in a collaborative effort from the National Space Development Agency (NASDA), Aerospace Engineering Laboratory (NAL), Mitsubishi Heavy Industries, and Ishikawajima-Harima.".
- LE-7 label "LE-7".
- LE-7 sameAs Q1050451.
- LE-7 sameAs Category:LE-7.
- LE-7 sameAs LE-7.
- LE-7 sameAs LE-7.
- LE-7 sameAs LE-7.
- LE-7 sameAs 미쓰비시_LE-7.
- LE-7 sameAs m.03mc4m1.
- LE-7 sameAs Q1050451.
- LE-7 sameAs LE-7火箭发动机.
- LE-7 wasDerivedFrom LE-7?oldid=699951174.
- LE-7 depiction LE-7_rocket_engine.jpg.
- LE-7 isPrimaryTopicOf LE-7.