CE-20
From Spacefaring
Q4272906
The CE-20 is a cryogenic rocket engine developed by the Liquid Propulsion Systems Centre (LPSC), a subsidiary of ISRO. It has been developed to power the upper stage of the LVM3. It is the first Indian cryogenic engine to feature a gas-generator cycle. The high thrust cryogenic engine is the most powerful upper stage cryogenic engine in operational service.
2015
Wikimedia, Wikidata
Persia, 2015, Ekran, Dong Fang Hong 2, cryogenic rocket engine, Tarshish, Sweden, Sikh Confederacy, Reman, Ashkenaz, Kingdom of Wolaita, Kingdom of Martabam-hongsawatoi, India, Havilah, Democratic Republic of the Congo, Chinland, Calvinist Republic of Ghent,
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Location: KML, Cluster Map, Maps,
| Type | Subtype | Date | Description | Notes | Source |
|---|---|---|---|---|---|
| commons | image | CE-20 engine for LVM3-M3 campaign going through 25 seconds long flight acceptance hot test at High Altitude Test facility of IPRC, Mahendragiri on 28 Oct 2022 | Commons | ||
| commons | image | CE20 Engine 640 second test Front | Commons | ||
| commons | image | CE20 Engine 640 second test Back | Commons | ||
| commons | image | CE20 Engine Interfaced with HAT facility | Commons | ||
| commons | image | CE20 Engine 001 | Commons | ||
| commons | image | C25 D Stage on test stand | Commons | ||
| commons | image | CE20 Engine 002 | Commons | ||
| commons | image | C25 D Stage hot test 003 | Commons | ||
| commons | image | C25 D Stage 640 second hot test | Commons | ||
| commons | image | C25 Development Stage hot test 001 | Commons | ||









