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- CE-7.5 abstract "The CE-7.5 is a cryogenic rocket engine developed by India 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 wikiPageRevisionID "599251861".
- 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 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 Liquid_hydrogen.
- CE-7.5 hasPhotoCollection CE-7.5.
- CE-7.5 length "2.14 m".
- CE-7.5 manufacturer Indian_Space_Research_Organisation.
- CE-7.5 name "CE-7.5".
- 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 subject Category:Hydrogen_rocket_engines.
- CE-7.5 subject Category:Rocket_engines.
- CE-7.5 subject Category:Space_programme_of_India.
- CE-7.5 comment "The CE-7.5 is a cryogenic rocket engine developed by India 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 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=599251861.
- CE-7.5 isPrimaryTopicOf CE-7.5.