M24
Engine · Japan
Original archive entry. The text, images and links below are kept as they were written.
Nissan solid rocket engine. Used on M-V launch vehicle. First flight 1997. M-V second stage.
Thrust (sl): 877.700 kN (197,315 lbf). Thrust (sl): 89,506 kgf. Chamber Pressure: 59.00 bar. Area Ratio: 31.