| Vehicle Overview Note: Payload performance and
estimated cost provided for information only. If you are interested in contracting
for launch services, we recommend that you contact the service provider directly using the
information above.
| |
LEO
Easterly Orbit
(63 deg. 200 km) |
LEO Polar Orbit
(90 deg., 200 km) |
Estimated Launch Price |
Launch Mass |
| Angara 1.1 |
4,400 lbm
2,000 kg |
3,750 lbm
1,700 kg |
? |
? |
| Angara 1.2 |
8,160 lbm
3,700 kg |
7,500 lbm
3,400 kg |
? |
? |
* Performance from
AIAA, "International Reference Guide to Space Launch
Systems", 3rd edition.
Vehicle Configuration
| |
Angara
Universal Module |
Briz
M Core |
| Length |
82 ft
25 m |
8.6 ft
2.61 m |
| Gross Mass |
309,000 lbm
130,000 kg |
14,480 lb
6,565 kg |
Propellant
Propellant Mass (estimated) |
LOX /
RG-1
287,000 lbm
130,000 kg |
N2O4 /
UDMH
10,950 lbm
4,965 kg |
Engine**
Thrust
Isp |
RD-191
471,000 lbf
2,095 kN
337.5 sec |
SS.98M
4,410 lbf
1,962 N
325.5 sec |
| Number of Engines |
1 |
1 + 4
vernier |
| Nominal Burn Time |
300 sec |
1000 sec
max |
** Note: Vacuum engine performance unless
otherwise specified.
|
