Soyuz ST-1
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
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.
Related
- Country
- Russia
- Engines
- RD-118
- Launch Vehicles
- Soyuz-FG, Soyuz-ST-B, Soyuz-2-1B, Soyuz ST / Fregat ST
- Propellants
- Lox/Kerosene