Dedicated launches

Glavkosmos offers its customers
the opportunity to use the full range
of Russian launch vehicles.

The implementation of dedicated missions
and the launch of payloads of any mass to the
required orbits is now available to our clients!

LV, type

ngara-1.2
Soyuz-2.1
Proton-M
Angara-A5

Lift-off mass, tons

171

311

702

770

Payload mass to LEO, tons

3,7

Up to 8,3

Up to 22,4

Up to 24

Launch site (spaceport)

Plesetsk, Vostochny

Plesetsk, Baikonur,
Vostochny

Baikonur

Plesetsk, Vostochny

First launch, year

2014

2006

2001

2014

 

LV ngara-1.2

 

  • 2014 First launch

Launch sites (spaceports):

Plesetsk, Vostochny

Number of stages:

2

Lift-off mass, tons:

171


Fuel components in I and II stages:

Liquid oxygen / kerosene


Payload mass, kg:

to LEO:  3700

 

LV Soyuz-2.1

Payload ascend part
incl. fregat upper stage
3rd stage
2rd stage
1rd stage
  • more than 1900 launches of the Soyuz LV, of which more than 100 – with the Fregat upper stage

  • RD-0124 Soyuz-2.1b has a NEW more powerful 3rd stage ENGINE (RD-0124)

LV dimensions, m:

length:  51.1
diameter:  10.3

Number of stages:

3

Lift-off mass, tons:

311

Fuel components in I, II, III stages:

Liquid oxygen / kerosene

Fuel for the Fregat upper stage:

unsymmetrical dimethylhydrazine / nitrogen tetroxide

Payload mass (Soyuz-2.1a / Soyuz-2.1b), kg:

to LEO:  7100 / 8300
to SSO:  4600 / 4900
to GTO:  1500 / 1800

 
  • more than 420 launches of this LV

LV Proton-M

1st stage

Six RD-276 liquid rocket engines

Flight time: 2 minutes

2st stage

Three RD-0210 and one RD-0211 liquid rocket engines

Flight time: 3.5 minutes

3st stage

One RD-0213 liquid rocket engine and one RD-0214 liquid rocket engine

Flight time: 4 minutes

Payload fairing & adapter stage

2 symmetrical payload fairing halves; multiple fairing lengths and diameters, adapter and separation system configurations are available

 

LV dimensions, m:

length:  56.2-58.2
with standard commercial 4.1 m diameter fairing

Number of stages:

3

Lift-off mass, tons:

702

Upper stage:

Breeze-M

Fairing external diameter/length, m:

with Breeze-M:  4.35 / 11.6
with Breeze-M:  4.35 / 15.255
with Breeze-M:  5.10 / 16.371
LEO module:  4.35 / 12.65

Fuel in all stages:

unsymmetrical dimethylhydrazine

Oxidant:

nitrogen tetroxide

Payload mass, kg:

to LEO:  22400
to GTO (with Breeze-M):  6300
to GEO (with Breeze-M):  3300

 
  • 2014 First launch

LV ngara-5

 

Launch sites (spaceports):

Plesetsk, Vostochny

Number of stages:

3

Lift-off mass, tons:

770

Fuel components in I, II III :

Liquid oxygen / kerosene

Payload mass, kg:

to LEO:  24000
to GTO:  5400
to GEO:  2800