CE-7.5
Sign in to saveThe 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 facts
- Subclass of
- cryogenic rocket engine
- Country of origin
- India
- Image
- Indigenous Cryogenic Upper Stage of GSLV-F09 at Stage Preparation Facility.jpg
via Wikidata · CC0
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Encyclopedic overview
6 sectionsContents
- Overview
- Specifications
- Development
- Applications
- See also
- References
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.
== Overview == CE-7.5 is a regeneratively-cooled, variable-thrust, fuel-rich staged combustion cycle rocket engine.
Excerpted from Wikipedia’s “CE-7.5” article, available under the CC BY-SA 4.0 licence.