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Soyuz ST-0
Part of R-7 Block BVGD stage series Family
LOx/Kerosene propellant rocket stage. Gross mass includes 1190 kg of hydrogen peroxide and 280 kg of liquid nitrogen expended during ascent but not contributing to propulsion.

Status: In production. Thrust: 1,021.10 kN (229,552 lbf). Gross mass: 44,400 kg (97,800 lb). Unfuelled mass: 3,810 kg (8,390 lb). Specific impulse: 310 s. Specific impulse sea level: 264 s. Burn time: 120 s. Height: 19.60 m (64.30 ft). Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft).



Country: Russia. Engines: RD-117. Launch Vehicles: Soyuz-FG, Soyuz-ST-B, Soyuz-2-1B, Soyuz ST / Fregat ST. Propellants: Lox/Kerosene.

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