Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Rocketdyne_H-1> ?p ?o }
- Rocketdyne_H-1 abstract "The Rocketdyne H-1 is a 205,000 lbf (910 kN) thrust liquid-propellant rocket engine burning LOX and RP-1. The H-1 was developed for use in the S-I and S-IB first stages of the Saturn I and Saturn IB rockets, respectively, where it was used in clusters of eight engines. After the Apollo program, surplus H-1 engines were rebranded and reworked as the Rocketdyne RS-27 engine with first usage on the Delta 2000 series in 1974.".
- Rocketdyne_H-1 thumbnail H-1_rocket_engine_diagram_image.jpg?width=300.
- Rocketdyne_H-1 wikiPageExternalLink 19740021163_1974021163.pdf.
- Rocketdyne_H-1 wikiPageID "713334".
- Rocketdyne_H-1 wikiPageLength "14029".
- Rocketdyne_H-1 wikiPageOutDegree "68".
- Rocketdyne_H-1 wikiPageRevisionID "679526250".
- Rocketdyne_H-1 wikiPageWikiLink Aerojet.
- Rocketdyne_H-1 wikiPageWikiLink Aerojet_General.
- Rocketdyne_H-1 wikiPageWikiLink Army_Ballistic_Missile_Agency.
- Rocketdyne_H-1 wikiPageWikiLink Booster_(rocketry).
- Rocketdyne_H-1 wikiPageWikiLink Category:Boeing.
- Rocketdyne_H-1 wikiPageWikiLink Category:North_American_Aviation.
- Rocketdyne_H-1 wikiPageWikiLink Category:Rocket_engines.
- Rocketdyne_H-1 wikiPageWikiLink Category:Rocketdyne_engines.
- Rocketdyne_H-1 wikiPageWikiLink Cruise_missile.
- Rocketdyne_H-1 wikiPageWikiLink DARPA.
- Rocketdyne_H-1 wikiPageWikiLink Delta_2000.
- Rocketdyne_H-1 wikiPageWikiLink Escape_velocity.
- Rocketdyne_H-1 wikiPageWikiLink Flight-qualify.
- Rocketdyne_H-1 wikiPageWikiLink Flight_qualify.
- Rocketdyne_H-1 wikiPageWikiLink Gas-generator_cycle.
- Rocketdyne_H-1 wikiPageWikiLink Gas-generator_cycle_(rocket).
- Rocketdyne_H-1 wikiPageWikiLink Gas_generator.
- Rocketdyne_H-1 wikiPageWikiLink HGM-25A_Titan_I.
- Rocketdyne_H-1 wikiPageWikiLink Heinz-Hermann_Koelle.
- Rocketdyne_H-1 wikiPageWikiLink J-2_(rocket_engine).
- Rocketdyne_H-1 wikiPageWikiLink Jupiter_missile.
- Rocketdyne_H-1 wikiPageWikiLink LOX.
- Rocketdyne_H-1 wikiPageWikiLink Liquid-propellant_rocket.
- Rocketdyne_H-1 wikiPageWikiLink Liquid_oxygen.
- Rocketdyne_H-1 wikiPageWikiLink Low_Earth_orbit.
- Rocketdyne_H-1 wikiPageWikiLink Low_earth_orbit.
- Rocketdyne_H-1 wikiPageWikiLink Marshall_Space_Flight_Center.
- Rocketdyne_H-1 wikiPageWikiLink NASA.
- Rocketdyne_H-1 wikiPageWikiLink North_American_Aviation.
- Rocketdyne_H-1 wikiPageWikiLink PGM-11_Redstone.
- Rocketdyne_H-1 wikiPageWikiLink PGM-17_Thor.
- Rocketdyne_H-1 wikiPageWikiLink PGM-19_Jupiter.
- Rocketdyne_H-1 wikiPageWikiLink RP-1.
- Rocketdyne_H-1 wikiPageWikiLink RS-27.
- Rocketdyne_H-1 wikiPageWikiLink Ramjet.
- Rocketdyne_H-1 wikiPageWikiLink Rocket_fuel.
- Rocketdyne_H-1 wikiPageWikiLink Rocket_propellant.
- Rocketdyne_H-1 wikiPageWikiLink Rocketdyne.
- Rocketdyne_H-1 wikiPageWikiLink Rocketdyne_E-1.
- Rocketdyne_H-1 wikiPageWikiLink Rocketdyne_J-2.
- Rocketdyne_H-1 wikiPageWikiLink Rocketdyne_S-3D.
- Rocketdyne_H-1 wikiPageWikiLink S-IB.
- Rocketdyne_H-1 wikiPageWikiLink S-IVB.
- Rocketdyne_H-1 wikiPageWikiLink SAE_International.
- Rocketdyne_H-1 wikiPageWikiLink SM-64_Navaho.
- Rocketdyne_H-1 wikiPageWikiLink SM-65_Atlas.
- Rocketdyne_H-1 wikiPageWikiLink Saturn_1B.
- Rocketdyne_H-1 wikiPageWikiLink Saturn_I.
- Rocketdyne_H-1 wikiPageWikiLink Saturn_IB.
- Rocketdyne_H-1 wikiPageWikiLink Saturn_I_(rocket).
- Rocketdyne_H-1 wikiPageWikiLink Specific_impulse.
- Rocketdyne_H-1 wikiPageWikiLink Sputnik_1.
- Rocketdyne_H-1 wikiPageWikiLink Titan_(rocket_family).
- Rocketdyne_H-1 wikiPageWikiLink Titan_missile.
- Rocketdyne_H-1 wikiPageWikiLink Turbopump.
- Rocketdyne_H-1 wikiPageWikiLink USA.
- Rocketdyne_H-1 wikiPageWikiLink US_Department_of_Defense.
- Rocketdyne_H-1 wikiPageWikiLink United_States.
- Rocketdyne_H-1 wikiPageWikiLink United_States_Department_of_Defense.
- Rocketdyne_H-1 wikiPageWikiLink V-2_rocket.
- Rocketdyne_H-1 wikiPageWikiLink Wernher_von_Braun.
- Rocketdyne_H-1 wikiPageWikiLink File:Comparison_of_Rocketdyne_S-3D_and_H-1_engines.jpg.
- Rocketdyne_H-1 wikiPageWikiLink File:H-1_rocket_engine_diagram.jpg.
- Rocketdyne_H-1 wikiPageWikiLink File:Saturn_I_test_article.jpg.
- Rocketdyne_H-1 wikiPageWikiLinkText "H-1".
- Rocketdyne_H-1 wikiPageWikiLinkText "Rocketdyne H-1".
- Rocketdyne_H-1 burnTime "155.0".
- Rocketdyne_H-1 caption "A cluster of 8 H-1 rocket engines lifted the Saturn I from the launch pad.".
- Rocketdyne_H-1 chamberPressure "700".
- Rocketdyne_H-1 combustionChamber "1".
- Rocketdyne_H-1 countryOfOrigin USA.
- Rocketdyne_H-1 countryOfOrigin United_States.
- Rocketdyne_H-1 cycle Gas-generator_cycle.
- Rocketdyne_H-1 cycle Gas-generator_cycle_(rocket).
- Rocketdyne_H-1 date "1963".
- Rocketdyne_H-1 diameter "4.9".
- Rocketdyne_H-1 dryWeight "2200.0".
- Rocketdyne_H-1 fuel RP-1.
- Rocketdyne_H-1 hasPhotoCollection Rocketdyne_H-1.
- Rocketdyne_H-1 imageSize "150".
- Rocketdyne_H-1 length "8.8".
- Rocketdyne_H-1 manufacturer Rocketdyne.
- Rocketdyne_H-1 name "H-1".
- Rocketdyne_H-1 oxidiser LOX.
- Rocketdyne_H-1 oxidiser Liquid_oxygen.
- Rocketdyne_H-1 purpose Booster_(rocketry).
- Rocketdyne_H-1 status "Retired".
- Rocketdyne_H-1 successor RS-27.
- Rocketdyne_H-1 thrust(sl)_ "205000".
- Rocketdyne_H-1 thrustToWeight "102.47".
- Rocketdyne_H-1 type "liquid".
- Rocketdyne_H-1 usedIn Saturn_1B.
- Rocketdyne_H-1 usedIn Saturn_I.