SRB-A
Engine · Japan
Original archive entry. The text, images and links below are kept as they were written.
Nissan solid rocket engine. In production. Monolithic motor, shorter than that for H-2, using Thiokol filament wound composite structure. First flight 2001.
Chamber Pressure: 118.00 bar. Area Ratio: 17.7. Propellant Formulation: HTPB.