Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/M-1_(rocket_engine)> ?p ?o }
- M-1_(rocket_engine) abstract "Aerojet's M-1 was the largest and most powerful liquid hydrogen-fueled liquid fuel rocket engine to be designed and component tested. The M-1 offered a baseline thrust of 6.67 million N (1.5 million lbf) and 8 million N (1.8 million lbf) as its immediate growth target. If built, the M-1 would be larger and more efficient than the famed F-1 that powered the first stage of the Saturn V rocket to the moon.".
- M-1_(rocket_engine) thumbnail M-1RocketEngineScale.png?width=300.
- M-1_(rocket_engine) wikiPageExternalLink 19730065121_1973065121.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19650018091_1965018091.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660002857_1966002857.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660004946_1966004946.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660006079_1966006079.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660007652_1966007652.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660009145_1966009145.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660009146_1966009146.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660009196_1966009196.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660009742_1966009742.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660010314_1966010314.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660010400_1966010400.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660012979_1966012979.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660014272_1966014272.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660014274_1966014274.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660016296_1966016296.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660017944_1966017944.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660018449_1966018449.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660019252_1966019252.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660022335_1966022335.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660023044_1966023044.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19660024687_1966024687.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19670008174_1967008174.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19670017909_1967017909.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19670020794_1967020794.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19670022113_1967022113.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19670028656_1967028656.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19670028658_1967028658.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19680006170_1968006170.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19680006392_1968006392.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19680006944_1968006944.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19680008719_1968008719.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19680008747_1968008747.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19680014530_1968014530.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19680021132_1968021132.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19690010477_1969010477.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 19720012802_1972012802.pdf.
- M-1_(rocket_engine) wikiPageExternalLink 6T3i4Kckv.
- M-1_(rocket_engine) wikiPageID "5006565".
- M-1_(rocket_engine) wikiPageLength "17252".
- M-1_(rocket_engine) wikiPageOutDegree "53".
- M-1_(rocket_engine) wikiPageRevisionID "650234111".
- M-1_(rocket_engine) wikiPageWikiLink Aerojet.
- M-1_(rocket_engine) wikiPageWikiLink Aerospike_engine.
- M-1_(rocket_engine) wikiPageWikiLink Service_Module.
- M-1_(rocket_engine) wikiPageWikiLink Apollo_program.
- M-1_(rocket_engine) wikiPageWikiLink Boeing_X-20_Dyna-Soar.
- M-1_(rocket_engine) wikiPageWikiLink Category:Rocket_engines_using_hydrogen_propellant.
- M-1_(rocket_engine) wikiPageWikiLink Dwight_D._Eisenhower.
- M-1_(rocket_engine) wikiPageWikiLink Expanding_nozzle.
- M-1_(rocket_engine) wikiPageWikiLink Gas-generator_cycle.
- M-1_(rocket_engine) wikiPageWikiLink HG-3_(rocket_engine).
- M-1_(rocket_engine) wikiPageWikiLink Helium.
- M-1_(rocket_engine) wikiPageWikiLink Horsepower.
- M-1_(rocket_engine) wikiPageWikiLink John_F._Kennedy.
- M-1_(rocket_engine) wikiPageWikiLink LGM-25C_Titan_II.
- M-1_(rocket_engine) wikiPageWikiLink LR-87.
- M-1_(rocket_engine) wikiPageWikiLink Liquid-propellant_rocket.
- M-1_(rocket_engine) wikiPageWikiLink Liquid_hydrogen.
- M-1_(rocket_engine) wikiPageWikiLink Liquid_oxygen.
- M-1_(rocket_engine) wikiPageWikiLink Low_Earth_orbit.
- M-1_(rocket_engine) wikiPageWikiLink Lunex_Project.
- M-1_(rocket_engine) wikiPageWikiLink Mars.
- M-1_(rocket_engine) wikiPageWikiLink Michoud,_New_Orleans.
- M-1_(rocket_engine) wikiPageWikiLink Michoud_Assembly_Facility.
- M-1_(rocket_engine) wikiPageWikiLink NASA.
- M-1_(rocket_engine) wikiPageWikiLink Newton_(unit).
- M-1_(rocket_engine) wikiPageWikiLink Nova_(rocket).
- M-1_(rocket_engine) wikiPageWikiLink Pound_(force).
- M-1_(rocket_engine) wikiPageWikiLink Rocketdyne_F-1.
- M-1_(rocket_engine) wikiPageWikiLink Rocketdyne_J-2.
- M-1_(rocket_engine) wikiPageWikiLink S-II.
- M-1_(rocket_engine) wikiPageWikiLink Saturn_V.
- M-1_(rocket_engine) wikiPageWikiLink Solid-fuel_rocket.
- M-1_(rocket_engine) wikiPageWikiLink Space_Launcher_System.
- M-1_(rocket_engine) wikiPageWikiLink Space_Shuttle.
- M-1_(rocket_engine) wikiPageWikiLink Space_Shuttle_main_engine.
- M-1_(rocket_engine) wikiPageWikiLink Specific_impulse.
- M-1_(rocket_engine) wikiPageWikiLink Turbopump.
- M-1_(rocket_engine) wikiPageWikiLink United_States.
- M-1_(rocket_engine) wikiPageWikiLink United_States_Air_Force.
- M-1_(rocket_engine) wikiPageWikiLink United_States_Army.
- M-1_(rocket_engine) wikiPageWikiLink Wernher_von_Braun.
- M-1_(rocket_engine) wikiPageWikiLink File:M-1_Rocket_Engine.jpg.
- M-1_(rocket_engine) wikiPageWikiLink File:M-1_rocket_turbopump.JPG.
- M-1_(rocket_engine) wikiPageWikiLinkText "M-1 (rocket engine)".
- M-1_(rocket_engine) wikiPageWikiLinkText "M-1 rocket engine".
- M-1_(rocket_engine) wikiPageWikiLinkText "M-1".
- M-1_(rocket_engine) caption "M-1 rocket engine specifications".
- M-1_(rocket_engine) chamberPressure "1000".
- M-1_(rocket_engine) countryOfOrigin United_States.
- M-1_(rocket_engine) cycle Gas-generator_cycle.
- M-1_(rocket_engine) diameter "4.28 m".
- M-1_(rocket_engine) dryWeight "9068.0".
- M-1_(rocket_engine) firstDate "Development abandoned at pre-prototype stage".
- M-1_(rocket_engine) fuel Liquid_hydrogen.
- M-1_(rocket_engine) imageSize "300".
- M-1_(rocket_engine) length "7.72 m".