Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/CE-20> ?p ?o }
Showing triples 1 to 80 of
80
with 100 triples per page.
- CE-20 abstract "The CE-20 is a cryogenic rocket engine being developed by the Liquid Propulsion Systems Centre, a subsidiary of Indian Space Research Organisation. It is being developed to power the upper stage of the Geosynchronous Satellite Launch Vehicle III. It is the first Indian cryogenic engine to feature a gas-generator cycle.".
- CE-20 thumbnail IndianCryoEngine25.JPG?width=300.
- CE-20 wikiPageExternalLink 48145813.cms.
- CE-20 wikiPageExternalLink IMG_0027.JPG.html.
- CE-20 wikiPageExternalLink IMG_0159.JPG.html.
- CE-20 wikiPageExternalLink citizens.htm.
- CE-20 wikiPageID "24110972".
- CE-20 wikiPageLength "4686".
- CE-20 wikiPageOutDegree "25".
- CE-20 wikiPageRevisionID "672379308".
- CE-20 wikiPageWikiLink CE-7.5.
- CE-20 wikiPageWikiLink Category:Rocket_engines.
- CE-20 wikiPageWikiLink Category:Rocket_engines_using_hydrogen_propellant.
- CE-20 wikiPageWikiLink Category:Space_programme_of_India.
- CE-20 wikiPageWikiLink Cryogenic_engine.
- CE-20 wikiPageWikiLink Cryogenic_rocket_engine.
- CE-20 wikiPageWikiLink GSAT-14.
- CE-20 wikiPageWikiLink GSLV_III.
- CE-20 wikiPageWikiLink Gas-generator_cycle.
- CE-20 wikiPageWikiLink Gas-generator_cycle_(rocket).
- CE-20 wikiPageWikiLink Geosynchronous_Satellite_Launch_Vehicle_Mk_III.
- CE-20 wikiPageWikiLink India.
- CE-20 wikiPageWikiLink Indian_Space_Research_Organisation.
- CE-20 wikiPageWikiLink LH2.
- CE-20 wikiPageWikiLink LOX.
- CE-20 wikiPageWikiLink Liquid_Propulsion_Systems_Centre.
- CE-20 wikiPageWikiLink Liquid_hydrogen.
- CE-20 wikiPageWikiLink Liquid_oxygen.
- CE-20 wikiPageWikiLink Specific_impulse.
- CE-20 wikiPageWikiLink Thrust-to-weight_ratio.
- CE-20 wikiPageWikiLinkText "CE-20".
- CE-20 wikiPageWikiLinkText "indigenous cryogenic engine".
- CE-20 caption "Model of CE-20".
- CE-20 chamberPressure "60.0".
- CE-20 combustionChamber "1".
- CE-20 countryOfOrigin India.
- CE-20 cycle Gas-generator_cycle.
- CE-20 cycle Gas-generator_cycle_(rocket).
- CE-20 date "2015".
- CE-20 designer Indian_Space_Research_Organisation.
- CE-20 dryWeight "588.0".
- CE-20 fuel LH2.
- CE-20 fuel Liquid_hydrogen.
- CE-20 hasPhotoCollection CE-20.
- CE-20 imageSize "250".
- CE-20 manufacturer Liquid_Propulsion_Systems_Centre.
- CE-20 name "CE-20".
- CE-20 nozzleRatio "100".
- CE-20 oxidiser LOX.
- CE-20 oxidiser Liquid_oxygen.
- CE-20 purpose "Upper stage booster".
- CE-20 status "Under Development".
- CE-20 thrust(vac)_ "200 kN".
- CE-20 type "liquid".
- CE-20 wikiPageUsesTemplate Template:Convert.
- CE-20 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- CE-20 wikiPageUsesTemplate Template:Reflist.
- CE-20 wikiPageUsesTemplate Template:Rocket_Engines.
- CE-20 wikiPageUsesTemplate Template:Rocketry-stub.
- CE-20 wikiPageUsesTemplate Template:Use_Indian_English.
- CE-20 subject Category:Rocket_engines.
- CE-20 subject Category:Rocket_engines_using_hydrogen_propellant.
- CE-20 subject Category:Space_programme_of_India.
- CE-20 hypernym Engine.
- CE-20 type Software.
- CE-20 type Program.
- CE-20 type Technology.
- CE-20 comment "The CE-20 is a cryogenic rocket engine being developed by the Liquid Propulsion Systems Centre, a subsidiary of Indian Space Research Organisation. It is being developed to power the upper stage of the Geosynchronous Satellite Launch Vehicle III. It is the first Indian cryogenic engine to feature a gas-generator cycle.".
- CE-20 label "CE-20".
- CE-20 sameAs सीई-२०.
- CE-20 sameAs CE-20.
- CE-20 sameAs CE-20.
- CE-20 sameAs m.07kh4m1.
- CE-20 sameAs சி.இ-20.
- CE-20 sameAs Q4272906.
- CE-20 sameAs Q4272906.
- CE-20 sameAs CE-20.
- CE-20 wasDerivedFrom CE-20?oldid=672379308.
- CE-20 depiction IndianCryoEngine25.JPG.
- CE-20 isPrimaryTopicOf CE-20.