Launch sites (spaceports):
Plesetsk, Vostochny
|
Glavkosmos offers its customers |
 |
 |
 |
 |
|
LV, type |
Àngara-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, |
Baikonur |
Plesetsk, Vostochny |
|
First launch, year |
2014 |
2006 |
2001 |
2014 |
LV Àngara-1.2
-
2014 First launch
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
incl. fregat upper stage
3rd stage
2nd stage
1st 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
2nd stage
Three RD-0210 and one RD-0211 liquid rocket engines
Flight time: 3.5 minutes
3rd 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 Àngara-À5
Launch sites (spaceports):
Plesetsk, Vostochny
Number of stages:
3
Lift-off mass, tons:
770
Fuel components in I, II è III ñòóïåíÿõ:
Liquid oxygen / kerosene
Payload mass, kg:
to LEO: 24000
to GTO: 5400
to GEO: 2800