Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/Rocketdyne_J-2> ?p ?o }
- Rocketdyne_J-2 nozzleRatio "27.5".
- Rocketdyne_J-2 oxidizer Liquid_oxygen.
- Rocketdyne_J-2 purpose "Upper stage engine".
- Rocketdyne_J-2 status "Retired".
- Rocketdyne_J-2 successor HG-3_(rocket_engine).
- Rocketdyne_J-2 successor J-2X.
- Rocketdyne_J-2 thrustToWeight "73.18".
- Rocketdyne_J-2 type "liquid".
- Rocketdyne_J-2 wikiPageUsesTemplate Template:Commons_category.
- Rocketdyne_J-2 wikiPageUsesTemplate Template:Convert.
- Rocketdyne_J-2 wikiPageUsesTemplate Template:Include-NASA.
- Rocketdyne_J-2 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- Rocketdyne_J-2 wikiPageUsesTemplate Template:J-2_(rocket_engine).
- Rocketdyne_J-2 wikiPageUsesTemplate Template:Main.
- Rocketdyne_J-2 wikiPageUsesTemplate Template:Project_Constellation.
- Rocketdyne_J-2 wikiPageUsesTemplate Template:Reflist.
- Rocketdyne_J-2 wikiPageUsesTemplate Template:Rocket_Engines.
- Rocketdyne_J-2 subject Category:Apollo_program_hardware.
- Rocketdyne_J-2 subject Category:North_American_Aviation.
- Rocketdyne_J-2 subject Category:Rocket_engines.
- Rocketdyne_J-2 subject Category:Rocket_engines_using_hydrogen_propellant.
- Rocketdyne_J-2 subject Category:Rocketdyne_engines.
- Rocketdyne_J-2 hypernym Engine.
- Rocketdyne_J-2 type Article.
- Rocketdyne_J-2 type Company.
- Rocketdyne_J-2 type Software.
- Rocketdyne_J-2 type Article.
- Rocketdyne_J-2 type Company.
- Rocketdyne_J-2 type Source.
- Rocketdyne_J-2 type Technology.
- Rocketdyne_J-2 comment "The J-2 was a liquid-fuel cryogenic rocket engine used on NASA's Saturn IB and Saturn V launch vehicles. Built in the U.S. by Rocketdyne, the J-2 burned cryogenic liquid hydrogen (LH2) and liquid oxygen (LOX) propellants, with each engine producing 1,033.1 kN (232,250 lbf) of thrust in vacuum. The engine's preliminary design dates back to recommendations of the 1959 Silverstein Committee.".
- Rocketdyne_J-2 label "Rocketdyne J-2".
- Rocketdyne_J-2 sameAs J-2_(motor_de_coet).
- Rocketdyne_J-2 sameAs J-2.
- Rocketdyne_J-2 sameAs J-2_(Raketentriebwerk).
- Rocketdyne_J-2 sameAs Motor_de_cohete_J-2.
- Rocketdyne_J-2 sameAs J-2_(rakettimoottori).
- Rocketdyne_J-2 sameAs J-2_(moteur-fusée).
- Rocketdyne_J-2 sameAs J-2.
- Rocketdyne_J-2 sameAs Rocketdyne_J-2.
- Rocketdyne_J-2 sameAs PWR_J-2.
- Rocketdyne_J-2 sameAs J-2ロケットエンジン.
- Rocketdyne_J-2 sameAs J-2_(silnik_rakietowy).
- Rocketdyne_J-2 sameAs J-2.
- Rocketdyne_J-2 sameAs m.034_q7.
- Rocketdyne_J-2 sameAs J-2.
- Rocketdyne_J-2 sameAs J-2.
- Rocketdyne_J-2 sameAs Rocketdyne_J-2.
- Rocketdyne_J-2 sameAs J-2_(raketmotor).
- Rocketdyne_J-2 sameAs Q967676.
- Rocketdyne_J-2 sameAs Q967676.
- Rocketdyne_J-2 sameAs J-2火箭发动机.
- Rocketdyne_J-2 wasDerivedFrom Rocketdyne_J-2?oldid=667049811.
- Rocketdyne_J-2 depiction J-2_test_firing.jpg.
- Rocketdyne_J-2 isPrimaryTopicOf Rocketdyne_J-2.