SLV-4
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 fourth stage.
Thrust (sl): 5.690 kN (1,279 lbf). Thrust (sl): 580 kgf. Chamber Pressure: 29.00 bar. Area Ratio: 31.