Encyclopedia Astronautica
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M-22
Part of M-10 Family
Nissan solid rocket engine.

Status: Retired 1984. Thrust: 285.00 kN (64,070 lbf). Gross mass: 9,800 kg (21,600 lb). Unfuelled mass: 2,607 kg (5,747 lb). Burn time: 66 s. Height: 5.00 m (16.40 ft). Diameter: 1.41 m (4.62 ft).

Country: Japan. Launch Vehicles: Mu-3C, Mu-3H, Mu-3S. Propellants: Solid. Stages: M-22. Agency: Nissan. More at: 9680.



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