PSLV-1
Engine · India
Original archive entry. The text, images and links below are kept as they were written.
ISRO solid rocket engine. Used on GSLV, PSLV. First flight 1993. GSLV first stage.
Thrust (sl): 4,363.000 kN (980,841 lbf). Thrust (sl): 444,905 kgf. Chamber Pressure: 58.00 bar. Area Ratio: 8.