H-2/J-1-1
Engine · Japan
Original archive entry. The text, images and links below are kept as they were written.
Nissan solid rocket engine. In Production. Used in J-1-1.
Thrust (sl): 1,414.000 kN (317,879 lbf). Thrust (sl): 144,194 kgf. Chamber Pressure: 58.00 bar. Area Ratio: 10.