Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/RD-270> ?p ?o }
Showing triples 1 to 77 of
77
with 100 triples per page.
- RD-270 abstract "RD-270 (Russian: Ра́кетный дв́игатель 270, Rocket Engine 270, 8D420) is a single chamber liquid bipropellant rocket engine designed by Energomash (USSR/Russia) in 1960–1970. It was to be used on the first stages of proposed heavy-lift UR-700 and UR-900 rocket families. It has the highest thrust among single chambered engines of USSR and Russia, 640 metric tons at the surface of Earth. The propellants used are unsymmetrical dimethylhydrazine (UDMH) and nitrogen tetroxide (N2O4). The chamber pressure is among the highest, being about 26 MPa. This was achieved by applying full flow staged combustion cycle for all the incoming mass of fuel, which is turned into a gas and passes through a couple of turbines before being burned in the combustion chamber. This allows it to achieve a specific impulse of 301 s (2.95 km/s) at the Earth's surface.The engine testing was underway when the decision was made to cancel the program. The development of it was stopped with all other work on corresponding rocket projects on 11 December 1970.".
- RD-270 wikiPageExternalLink rd270.htm.
- RD-270 wikiPageID "11463948".
- RD-270 wikiPageLength "6122".
- RD-270 wikiPageOutDegree "50".
- RD-270 wikiPageRevisionID "702245919".
- RD-270 wikiPageWikiLink Category:Rocket_engines_of_the_Soviet_Union.
- RD-270 wikiPageWikiLink Category:Rocket_engines_using_hypergolic_propellant.
- RD-270 wikiPageWikiLink Combustion_chamber.
- RD-270 wikiPageWikiLink Dinitrogen_tetroxide.
- RD-270 wikiPageWikiLink Liquid-propellant_rocket.
- RD-270 wikiPageWikiLink Liquid_oxygen.
- RD-270 wikiPageWikiLink N1_(rocket).
- RD-270 wikiPageWikiLink NPO_Energomash.
- RD-270 wikiPageWikiLink Pascal_(unit).
- RD-270 wikiPageWikiLink Pentaborane.
- RD-270 wikiPageWikiLink Pounds_per_square_inch.
- RD-270 wikiPageWikiLink Proton_(rocket_family).
- RD-270 wikiPageWikiLink R-56_(rocket).
- RD-270 wikiPageWikiLink RD-170.
- RD-270 wikiPageWikiLink RD-253.
- RD-270 wikiPageWikiLink RP-1.
- RD-270 wikiPageWikiLink Rocket_engine.
- RD-270 wikiPageWikiLink Rocketdyne_F-1.
- RD-270 wikiPageWikiLink Russia.
- RD-270 wikiPageWikiLink Soviet_Union.
- RD-270 wikiPageWikiLink Specific_impulse.
- RD-270 wikiPageWikiLink Staged_combustion_cycle.
- RD-270 wikiPageWikiLink Ukraine.
- RD-270 wikiPageWikiLink Universal_Rocket.
- RD-270 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- RD-270 wikiPageWikiLink Valentin_Glushko.
- RD-270 wikiPageWikiLink Zirconium_dioxide.
- RD-270 wikiPageWikiLinkText "RD-214".
- RD-270 wikiPageWikiLinkText "RD-270".
- RD-270 wikiPageWikiLinkText "RD-270M".
- RD-270 caption "Photo of rocket engine RD-270 exhibited for viewers.".
- RD-270 chamberPressure "3828.0".
- RD-270 countryOfOrigin Russia.
- RD-270 countryOfOrigin Soviet_Union.
- RD-270 cycle Staged_combustion_cycle.
- RD-270 date "1969".
- RD-270 designer Soviet_Union.
- RD-270 designer Ukraine.
- RD-270 designer Valentin_Glushko.
- RD-270 fuel Unsymmetrical_dimethylhydrazine.
- RD-270 imageSize "250".
- RD-270 manufacturer NPO_Energomash.
- RD-270 name "RD-270".
- RD-270 oxidiser Dinitrogen_tetroxide.
- RD-270 status "Retired".
- RD-270 successor "RD-270M".
- RD-270 type "liquid".
- RD-270 usedIn "1".
- RD-270 weight "120.0".
- RD-270 wikiPageUsesTemplate Template:Citation_needed.
- RD-270 wikiPageUsesTemplate Template:Convert.
- RD-270 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- RD-270 wikiPageUsesTemplate Template:Lang-ru.
- RD-270 wikiPageUsesTemplate Template:Reflist.
- RD-270 wikiPageUsesTemplate Template:Rocket_Engines.
- RD-270 subject Category:Rocket_engines_of_the_Soviet_Union.
- RD-270 subject Category:Rocket_engines_using_hypergolic_propellant.
- RD-270 hypernym Engine.
- RD-270 type Software.
- RD-270 type Redirect.
- RD-270 comment "RD-270 (Russian: Ра́кетный дв́игатель 270, Rocket Engine 270, 8D420) is a single chamber liquid bipropellant rocket engine designed by Energomash (USSR/Russia) in 1960–1970. It was to be used on the first stages of proposed heavy-lift UR-700 and UR-900 rocket families. It has the highest thrust among single chambered engines of USSR and Russia, 640 metric tons at the surface of Earth. The propellants used are unsymmetrical dimethylhydrazine (UDMH) and nitrogen tetroxide (N2O4).".
- RD-270 label "RD-270".
- RD-270 sameAs Q4386506.
- RD-270 sameAs RD-270.
- RD-270 sameAs RD-270.
- RD-270 sameAs m.02rdpfn.
- RD-270 sameAs РД-270.
- RD-270 sameAs РД-270.
- RD-270 sameAs Q4386506.
- RD-270 wasDerivedFrom RD-270?oldid=702245919.
- RD-270 isPrimaryTopicOf RD-270.