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M-20
Part of M-10
Nissan solid rocket engine.

Status: Retired 1972. Thrust: 285.00 kN (64,070 lbf). Gross mass: 9,900 kg (21,800 lb). Unfuelled mass: 2,779 kg (6,126 lb). Burn time: 66 s. Height: 4.70 m (15.40 ft). Diameter: 1.41 m (4.62 ft).

Country: Japan. Launch Vehicles: Mu-1, Mu-3D, Mu-4S, ETV. Propellants: Solid. Stages: M-20. Agency: Nissan.
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