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-1” middle class launch vehicle

Soyuz-1” launch vehicle is two-stage middle class launch vehicle developed for spacecraft launches from launching facilities  which are meant for “Soyuz-2” launch vehicle.

 

Middle class launch vehicle development associates with growing needs of small spacecraft launches.

“Soyuz-1” is under the development on the basis of “Soyuz-2-1b” launch vehicle by boosters removal, engine NK-33-1 mounting on the central module and Nose Fairing usage of “Soyuz” launch vehicle.

 

Draft design for “Soyuz-1” launch vehicle has been developed.

 

Specifications of “Soyuz-1” launch vehicle

Number of stages

2

Liftoff mass

158 t

Maximal length

44 m

Nose Fairing diameter

3 m
 

 ”Soyuz-1” launch vehicle power capacity

Launching site

Baikonur

Plesetsk

Low circular orbit
(
mean altitude ~200 km)

2 850 kg
(
inclination 51,8º)

2 800 kg

(inclination 62,8º)