M-V-4
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.
Chamber Pressure: 49.00 bar. Area Ratio: 89.
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.
Chamber Pressure: 49.00 bar. Area Ratio: 89.