Encyclopedia entry

M14

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 first stage.

Thrust (sl): 3,369.400 kN (757,471 lbf). Thrust (sl): 343,587 kgf. Chamber Pressure: 59.00 bar. Area Ratio: 11.

Subtopics

M24 Nissan solid rocket engine. Used on M-V launch vehicle. First flight 1997. M-V second stage.
SRB-A Nissan solid rocket engine. In production. Monolithic motor, shorter than that for H-2, using Thiokol filament wound composite structure. First flight 2001.