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Soyuz M-0
Part of R-7 Block BVGD stage series Family
LOx/Kerosene propellant rocket stage. .

Status: Development ended 2000. Thrust: 872.00 kN (196,033 lbf). Gross mass: 42,200 kg (93,000 lb). Unfuelled mass: 3,000 kg (6,600 lb). Specific impulse: 336 s. Specific impulse sea level: 298 s. Burn time: 145 s. Height: 20.00 m (65.00 ft). Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft).



Country: Russia. Engines: RD-120K. Launch Vehicles: Soyuz M. Propellants: Lox/Kerosene.

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