M-3B-Mu
Engine · Japan
Original archive entry. The text, images and links below are kept as they were written.
Nissan solid rocket engine. Used on Mu-3S launch vehicle. First flight 1969.
Chamber Pressure: 42.00 bar. Area Ratio: 52.
Subtopics
- M-3B-J Nissan solid rocket engine. In development. Used on J-1 launch vehicle. First flight 1996.