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Soyuz ST-2
Part of R-7 Block I stage series Family
LOx/Kerosene propellant rocket stage. .

Status: In production. Thrust: 294.00 kN (66,093 lbf). Gross mass: 25,200 kg (55,500 lb). Unfuelled mass: 2,355 kg (5,191 lb). Specific impulse: 359 s. Burn time: 300 s. Height: 6.74 m (22.11 ft). Diameter: 2.66 m (8.72 ft). Span: 2.66 m (8.72 ft).



Country: Russia. Engines: RD-0124. Launch Vehicles: Soyuz-FG, Soyuz-ST-B, Soyuz-2-1B, Soyuz ST / Fregat ST. Propellants: Lox/Kerosene.

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