SLV-2
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 second stage.
Thrust (sl): 216.000 kN (48,558 lbf). Thrust (sl): 22,026 kgf. Chamber Pressure: 43.00 bar. Area Ratio: 14.
Subtopics
- SLV-3 engine ISRO solid rocket engine. Used on ASLV, SLV. First flight 1979. ASLV third stage.