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SOYUZ-5 Launch Vehicle
A promising two-stage medium-lift launch vehicle Soyuz-5 is under development to inject automated spacecraft into sun-synchronous, high elliptical, geotransfer, and geostationary orbits using also an upper stage where necessary.
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SOYUZ-5 Launch Vehicle
A promising two-stage medium-lift launch vehicle Soyuz-5 is under development to inject automated spacecraft into sun-synchronous, high elliptical, geotransfer, and geostationary orbits using also an upper stage where necessary.
SOYUZ-5 Launch Vehicle
A promising two-stage medium-lift launch vehicle, Soyuz-5, is under development with the purpose of launching automatic spacecraft into sun-synchronous, high elliptical, geotransfer, and geostationary orbits including cases when the upper stage is used, and the launches of manned spacecraft.
SOYUZ-5 Launch Vehicle
Performance
Number of stages |
2 |
|
Total length (manned / unmanned) |
65.908 / 63.706 m |
|
Nose fairing diameter |
4.11; 4.35; 5.2 m |
|
Fuel |
Oxidizer |
Liquid oxygen |
Propellant |
Naphthyl |
|
Payload mass to inject into LEO: - i=51.7°, Нπ × Нα = minus 1,690 × 250 km - i=51.7°, Нπ × Нα = minus 140 × 200 km |
17.0 t
14.4 t |
|
Launch site |
Baikonur, Sea Launch |