CE-7. 5
| Use attributes for filter ! | |
| First flight | 15 April 2010 (failure); 5 January 2014 (success) |
|---|---|
| Thrust (vac.) | 73. 5 kN (16,500 lbf) |
| Chamber | 1 |
| Chamber pressure | 5. 8 MPa (58 bar) / 7. 5 MPa (75 bar) |
| Designers | LPSC |
| Indian Space Research Organisation | |
| Manufacturers | Hindustan Aeronautics Limited |
| Indian Space Research Organisation | |
| Date of Reg. | |
| Date of Upd. | |
| ID | 2981047 |
About CE-7. 5
The CE-7. 5 is a cryogenic rocket engine developed by the Indian Space Research Organisation 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. It replaced the KVD-1 Russian cryogenic engine that powered the upper stage of GSLV Mk-1.