Matches in DBpedia 2015-10 for { <http://dbpedia.org/resource/CE-7.5> ?p ?o }
Showing triples 1 to 72 of
72
with 100 triples per page.
- CE-7.5 abstract "The CE-7.5 is a cryogenic rocket engine developed by ISRO to power the upper stage of its GSLV Mk-2 launch vehicle. The engine was developed as a part of the Cryogenic Upper Stage Project (CUSP). It replaced the KVD-1 (RD-56) Russian cryogenic engine that powered the upper stage of GSLV Mk-1.".
- CE-7.5 wikiPageID "24321439".
- CE-7.5 wikiPageLength "5206".
- CE-7.5 wikiPageOutDegree "21".
- CE-7.5 wikiPageRevisionID "663626690".
- CE-7.5 wikiPageWikiLink CE-20.
- CE-7.5 wikiPageWikiLink Category:Rocket_engines.
- CE-7.5 wikiPageWikiLink Category:Rocket_engines_using_hydrogen_propellant.
- CE-7.5 wikiPageWikiLink Category:Space_programme_of_India.
- CE-7.5 wikiPageWikiLink Cryogenic_rocket_engine.
- CE-7.5 wikiPageWikiLink GSAT-14.
- CE-7.5 wikiPageWikiLink GSLV.
- CE-7.5 wikiPageWikiLink Geosynchronous_Satellite_Launch_Vehicle.
- CE-7.5 wikiPageWikiLink ISRO.
- CE-7.5 wikiPageWikiLink India.
- CE-7.5 wikiPageWikiLink Indian_Space_Research_Organisation.
- CE-7.5 wikiPageWikiLink KVD-1.
- CE-7.5 wikiPageWikiLink LH2.
- CE-7.5 wikiPageWikiLink LOX.
- CE-7.5 wikiPageWikiLink Liquid_Propulsion_Systems_Centre.
- CE-7.5 wikiPageWikiLink Liquid_hydrogen.
- CE-7.5 wikiPageWikiLink Liquid_oxygen.
- CE-7.5 wikiPageWikiLink Staged_combustion_cycle.
- CE-7.5 wikiPageWikiLink Staged_combustion_cycle_(rocket).
- CE-7.5 wikiPageWikiLinkText "CE-7.5".
- CE-7.5 wikiPageWikiLinkText "Indian cryogenic engine".
- CE-7.5 wikiPageWikiLinkText "cryogenic third stage".
- CE-7.5 chamberPressure "5.8".
- CE-7.5 combustionChamber "1".
- CE-7.5 countryOfOrigin India.
- CE-7.5 cycle Staged_combustion_cycle.
- CE-7.5 cycle Staged_combustion_cycle_(rocket).
- CE-7.5 date "2002".
- CE-7.5 designer Liquid_Propulsion_Systems_Centre.
- CE-7.5 diameter "1.56 m".
- CE-7.5 dryWeight "435.0".
- CE-7.5 fuel LH2.
- CE-7.5 fuel Liquid_hydrogen.
- CE-7.5 hasPhotoCollection CE-7.5.
- CE-7.5 length "2.14 m".
- CE-7.5 manufacturer ISRO.
- CE-7.5 manufacturer Indian_Space_Research_Organisation.
- CE-7.5 name "CE-7.5".
- CE-7.5 oxidiser LOX.
- CE-7.5 oxidiser Liquid_oxygen.
- CE-7.5 purpose "Upper-stage booster".
- CE-7.5 status "In use".
- CE-7.5 thrust(vac)_ "73.5 kN".
- CE-7.5 type "liquid".
- CE-7.5 wikiPageUsesTemplate Template:Cn.
- CE-7.5 wikiPageUsesTemplate Template:Convert.
- CE-7.5 wikiPageUsesTemplate Template:Infobox_rocket_engine.
- CE-7.5 wikiPageUsesTemplate Template:Portal.
- CE-7.5 wikiPageUsesTemplate Template:Reflist.
- CE-7.5 wikiPageUsesTemplate Template:Rocket_Engines.
- CE-7.5 wikiPageUsesTemplate Template:Use_Indian_English.
- CE-7.5 subject Category:Rocket_engines.
- CE-7.5 subject Category:Rocket_engines_using_hydrogen_propellant.
- CE-7.5 subject Category:Space_programme_of_India.
- CE-7.5 hypernym Engine.
- CE-7.5 type Software.
- CE-7.5 type Program.
- CE-7.5 type Technology.
- CE-7.5 comment "The CE-7.5 is a cryogenic rocket engine developed by ISRO to power the upper stage of its GSLV Mk-2 launch vehicle. The engine was developed as a part of the Cryogenic Upper Stage Project (CUSP). It replaced the KVD-1 (RD-56) Russian cryogenic engine that powered the upper stage of GSLV Mk-1.".
- CE-7.5 label "CE-7.5".
- CE-7.5 sameAs CE-7.5.
- CE-7.5 sameAs CE-7.5.
- CE-7.5 sameAs m.07k8_bx.
- CE-7.5 sameAs Q5010171.
- CE-7.5 sameAs Q5010171.
- CE-7.5 wasDerivedFrom CE-7.5?oldid=663626690.
- CE-7.5 isPrimaryTopicOf CE-7.5.