UM-129A
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 H-1-3.
Thrust (sl): 58.600 kN (13,174 lbf). Thrust (sl): 5,973 kgf. Area Ratio: 54.
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 H-1-3.
Thrust (sl): 58.600 kN (13,174 lbf). Thrust (sl): 5,973 kgf. Area Ratio: 54.