CE-20
| Use attributes for filter ! | |
| Manufacturers | Hindustan Aeronautics Limited |
|---|---|
| First flight | June 5, 2017 |
| Thrust (vac.) | 200 kN (45,000 lbf) |
| Nozzle ratio | 100 |
| Cycle | Gas Generator |
| Mixture ratio | 5. 05 |
| Date of Reg. | |
| Date of Upd. | |
| ID | 2981056 |
About CE-20
The CE-20 is a cryogenic rocket engine developed by the Liquid Propulsion Systems Centre, a subsidiary of Indian Space Research Organisation. It has been developed to power the upper stage of the Geosynchronous Satellite Launch Vehicle Mk III. It is the first Indian cryogenic engine to feature a gas-generator cycle.