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M-100-100
Russian solid rocket engine. M-100 second stage.

AKA: M-100-2. Status: Retired 1993. Gross mass: 100 kg (220 lb). Unfuelled mass: 55 kg (121 lb). Burn time: 4.50 s. Height: 1.60 m (5.20 ft). Diameter: 0.25 m (0.82 ft).

Country: Russia. Launch Vehicles: M-100, M-100 (A-1), M-100B, M-100A. Propellants: Solid. Stages: M-100-100. Agency: MO.
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