BANNER_RIGHT
 
RAZDEL

"R-7" family launch vehicles

"Soyuz-FG" launch vehicle

"Vostok" launch vehicle

"Molniya" launch vehicle

"Voskhod" launch vehicle

"Soyuz-2" launch vehicle

"Soyuz-U" launch vehicle

"Ikar" injection module

"Soyuz"-series launch vehicles

"Soyuz-ST" launch vehicle

"Soyuz-2-3" launch vehicle

"Soyuz-1" launch vehicle

Launch statistics

 

 

 

"Soyuz-ST" launch vehicle

"Soyuz-ST” launch vehicle is developed on the bases of “Sayuz-2” launch vehicle and design for commercial spacecraft launches from Kourou launching site (French Guiana).

 

“Soyuz-ST” launch vehicle is adapted in compliance with the requirements of Kourou Space Centre in terms of safety (uplink commands to stop the flight), telemetry system (UHF transmitters with European IRIG format for telemetry frame) operational environment (high humidity, sea transportation and others).

 

“Soyuz-ST” launch vehicle is equipped with ST-type Nose Fairing, meeting international demands. When used with “Fregat” kick stage it will enable to orbit a wide range of Payloads.

 

Power capacity of “Soyuz-ST” launch vehicle

Launch vehicle

"Soyuz-ST-A"

"Soyuz-ST-B"

Geo-transfer orbit

(ΔV=1500 mps)

2850 kg

3240 kg

Sun-synchronous orbit  

(Íêð=820 km)

4230 kg

4900 kg