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Soyuz M-3
Part of Block L Family
LOx/Kerosene propellant rocket stage. Empty mass estimated. Multiple restart engine.

Status: Development ended 2000. Thrust: 20.00 kN (4,496 lbf). Gross mass: 5,000 kg (11,000 lb). Unfuelled mass: 1,000 kg (2,200 lb). Specific impulse: 360 s. Burn time: 700 s. Height: 2.70 m (8.80 ft). Diameter: 2.40 m (7.80 ft). Span: 2.40 m (7.80 ft).



Country: Russia. Engines: RD-161-1. Launch Vehicles: Soyuz M. Propellants: Lox/Kerosene.

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