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-U" launch vehicle

 

"Soyuz-U" unified middle-class launch vehicle is intended for injection of "Soyuz"-type and "Progress"-type manned and cargo spaceships into near-earth orbit, spacecraft for special purposes ("Kosmos"-series spacecraft), spacecraft for national economy ("Resurs-F"-type spacecraft), spacecraft for space technology research and spacecraft for medical and biological purposes ("Foton"-type and "Bion"-type spacecraft ), as well as foreign spacecraft.

 

"Soyuz-U" launch vehicle can be equipped with nose fairing of the following diameters: 2,7; 3,0; 3,3; 3,7 m.

 

The confirmed serviceability index of "Soyuz-U" launch vehicle is 0,983.

 

"Soyuz-U" launch vehicle power potentialities

(with 3,3 m nose fairing)

 

Launch site

Inclination (degree)

Circular orbit average altitude (km)

Injected payload mass (kg)

Plesetsk62,8220 6700
67,1190 6640
81,4200 6200
Baikonur51,6200 6950
64,9190 6660
70,4200 6590