PSLV-3
Engine · India
Original archive entry. The text, images and links below are kept as they were written.
ISRO solid rocket engine. Used on PSLV launch vehicle. First flight 1993.
Thrust (sl): 180.700 kN (40,623 lbf). Thrust (sl): 18,430 kgf. Chamber Pressure: 63.00 bar. Area Ratio: 52.
Subtopics
- Agni3 S2 DRDO solid rocket engine. Agni 3 second stage.
- Agni 3 engine DRDO solid rocket engine. Agni 3 first stage.