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Soyuz ST-1


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z Soyuz ST-1 Part of R-7 Block A stage series LOx/Kerosene propellant rocket stage. Gross mass includes 2600 kg of hydrogen peroxide and 520 kg of liquid nitrogen expended during ascent but not contributing to propulsion.

Status: In production. Thrust: 999.60 kN (224,719 lbf). Gross mass: 105,400 kg (232,300 lb). Unfuelled mass: 6,875 kg (15,156 lb). Specific impulse: 311 s. Specific impulse sea level: 245 s. Burn time: 286 s. Height: 27.80 m (91.20 ft). Diameter: 2.95 m (9.67 ft). Span: 2.95 m (9.67 ft).

Country: Russia. Engines: RD-118. Launch Vehicles: Soyuz-FG, Soyuz-ST-B, Soyuz-2-1B, Soyuz ST / Fregat ST. Propellants: Lox/Kerosene. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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