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M-3B-Mu
Nissan solid rocket engine. Used on Mu-3S launch vehicle. First flight 1969.

AKA: M-3B. Status: In development. Number: 24 . Thrust: 132.10 kN (29,697 lbf). Gross mass: 3,590 kg (7,910 lb). Unfuelled mass: 490 kg (1,080 lb). Specific impulse: 294 s. Burn time: 85 s. Height: 2.68 m (8.79 ft). Diameter: 1.50 m (4.90 ft).

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.
Country: Japan. Launch Vehicles: Mu-3S, Mu-3S-II, J-1, J-1 F2. Propellants: Solid. Stages: M-3B-J, M-3B-Mu. Agency: Nissan.
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