Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/CE-20> ?p ?o }
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- 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 Mk III. It is the first Indian cryogenic engine to feature a gas-generator cycle.".
- CE-20 thumbnail IndianCryoEngine25.JPG?width=300.
- CE-20 wikiPageExternalLink IMG_0027.JPG.html.
- CE-20 wikiPageExternalLink citizens.htm.
- CE-20 wikiPageExternalLink 48145813.cms.
- CE-20 wikiPageExternalLink IMG_0159.JPG.html.
- CE-20 wikiPageExternalLink article8258313.ece.
- CE-20 wikiPageID "24110972".
- CE-20 wikiPageLength "5282".
- CE-20 wikiPageOutDegree "26".
- CE-20 wikiPageRevisionID "706062600".
- CE-20 wikiPageWikiLink CE-7.5.
- CE-20 wikiPageWikiLink Category:Rocket_engines.
- CE-20 wikiPageWikiLink Category:Rocket_engines_of_India.
- CE-20 wikiPageWikiLink Category:Rocket_engines_using_hydrogen_propellant.
- CE-20 wikiPageWikiLink Cryogenic_rocket_engine.
- CE-20 wikiPageWikiLink GSAT-14.
- CE-20 wikiPageWikiLink Gas-generator_cycle.
- CE-20 wikiPageWikiLink Geosynchronous_Satellite_Launch_Vehicle_Mk_III.
- CE-20 wikiPageWikiLink Hindustan_Aeronautics_Limited.
- CE-20 wikiPageWikiLink India.
- CE-20 wikiPageWikiLink Indian_Space_Research_Organisation.
- 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 combustionChamber "1".
- CE-20 countryOfOrigin India.
- CE-20 cycle Gas-generator_cycle.
- CE-20 date "2015".
- CE-20 designer Indian_Space_Research_Organisation.
- CE-20 designer Liquid_Propulsion_Systems_Centre.
- CE-20 dryWeight "588.0".
- CE-20 fuel Liquid_hydrogen.
- CE-20 imageSize "250".
- CE-20 manufacturer Hindustan_Aeronautics_Limited.
- CE-20 name "CE-20".
- CE-20 nozzleRatio "100".
- CE-20 oxidiser Liquid_oxygen.
- CE-20 purpose "Upper stage booster".
- CE-20 status "Under Development".
- 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_of_India.
- CE-20 subject Category:Rocket_engines_using_hydrogen_propellant.
- 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 Mk III. It is the first Indian cryogenic engine to feature a gas-generator cycle.".
- CE-20 label "CE-20".
- CE-20 sameAs Q4272906.
- 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 CE-20.
- CE-20 wasDerivedFrom CE-20?oldid=706062600.
- CE-20 depiction IndianCryoEngine25.JPG.
- CE-20 isPrimaryTopicOf CE-20.