Matches in DBpedia 2014 for { <http://dbpedia.org/resource/M-1_(rocket_engine)> ?p ?o. }
Showing items 1 to 66 of
66
with 100 items per page.
- M-1_(rocket_engine) abstract "Aerojet's M-1 was the largest and most powerful liquid hydrogen-fueled 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 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 19730065121_1973065121.pdf.
- M-1_(rocket_engine) wikiPageID "5006565".
- M-1_(rocket_engine) wikiPageRevisionID "606369981".
- 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) firstDate "Development abandoned at pre-prototype stage".
- M-1_(rocket_engine) fuel Liquid_hydrogen.
- M-1_(rocket_engine) hasPhotoCollection M-1_(rocket_engine).
- M-1_(rocket_engine) imageSize "300".
- M-1_(rocket_engine) manufacturer Aerojet.
- M-1_(rocket_engine) name "M-1".
- M-1_(rocket_engine) oxidiser Liquid_oxygen.
- M-1_(rocket_engine) status "Abandoned in development stage.".
- M-1_(rocket_engine) thrust(sl)_ "1500000".
- M-1_(rocket_engine) type "liquid".
- M-1_(rocket_engine) subject Category:Hydrogen_rocket_engines.
- M-1_(rocket_engine) comment "Aerojet's M-1 was the largest and most powerful liquid hydrogen-fueled 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) label "M-1 (rocket engine)".
- M-1_(rocket_engine) label "M-1 (ロケットエンジン)".
- M-1_(rocket_engine) sameAs M-1_(ロケットエンジン).
- M-1_(rocket_engine) sameAs m.0czj6d.
- M-1_(rocket_engine) sameAs Q6711969.
- M-1_(rocket_engine) sameAs Q6711969.
- M-1_(rocket_engine) wasDerivedFrom M-1_(rocket_engine)?oldid=606369981.
- M-1_(rocket_engine) depiction M-1RocketEngineScale.png.
- M-1_(rocket_engine) isPrimaryTopicOf M-1_(rocket_engine).