SLV-3 engine
Engine · India
Original archive entry. The text, images and links below are kept as they were written.
ISRO solid rocket engine. Used on ASLV, SLV. First flight 1979. ASLV third stage.
Thrust (sl): 62.200 kN (13,983 lbf). Thrust (sl): 6,344 kgf. Chamber Pressure: 43.00 bar. Area Ratio: 24.
Related
- Country
- India
- Propellants
- Solid
- Stages
- SLV-3 engine
- Agency
- ISRO