Q5010171: Difference between revisions
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Q5010171
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{{Page|CE-7.5|Classes|cryogenic rocket engine developed by the Indian Space Research Organisation}} | {{Page|CE-7.5|Classes|cryogenic rocket engine developed by the Indian Space Research Organisation|}} | ||
Latest revision as of 16:02, 17 February 2025
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.
Wikidata
India,
Ashkenaz, Calvinist Republic of Ghent, Chinland, Democratic Republic of the Congo, Havilah, India, Kingdom of Martabam-hongsawatoi, Kingdom of Wolaita, Persia, Reman, Sikh Confederacy, Tarshish, cryogenic rocket engine, Dong Fang Hong 2, Ekran, Republic of Haiti,
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Location: KML, Cluster Map, Maps,
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