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 Payload*
(51.6 degree inclination, 200 km) |
Sun Synch Payload* |
Estimated Launch Price |
Configuration |
Launch Mass |
| Soyuz |
15,400 lb
7,000 kg |
--- |
US $35 M |
Basic Vehicle |
683,000 lb
310,000 kg |
| Soyuz Ikar |
7,700 lb
3,500 kg |
6,600 lb
3,000 kg |
US $35 M |
Basic Vehicle
+ Ikar 3rd Stage |
683,000 lb
310,000 kg |
| Molniya |
--- |
5,500 lb
2,500 kg |
US $40 M |
Basic Vehicle
+ 3rd Stage |
672,000 lb
305,000 kg |
| Soyuz 2 |
18,500 lb
8,400 kg |
--- |
US $40 M |
Upgraded Basic Vehicle |
683,000 lb
310,000 kg |
| Soyuz Fregat |
--- |
10,560 lb
4,800 kg |
US $45 M |
Upgraded Basic Vehicle + 3rd
Stage |
672,000 lb
305,000 kg |
* Performance values from STARSEM Website
Vehicle Overview
| |
Liquid Strap-Ons
(4 Total) |
Stage 1
(Core) |
Stage 2 |
Stage 3
(Molniya) |
| Length |
64.3 ft
19.6 m |
91.2 ft
27.8 m |
22.1 ft
6.7 m |
8.7 ft
2.6 m |
| Diameter |
8.8 ft
2.7 m |
7.1 to 9.7 ft
2.15 to 2.95 m |
8.7 ft
2.6 m |
7.9 ft
2.4 m |
| Gross Mass |
94,200 lb
42,750 kg |
223,000 lb
101,000 kg |
56,000 lb
25,400 kg |
9,900 lb
4,500 kg |
Propellant
Propellant Mass |
LOX / RP
86,400 lb
39,200 kg |
LOX / RP
208,000 lb
94,500 kg |
LOX / RP
50,700 lb
23,000 kg |
LOX / RP
7,600 lb
3,450 kg |
Engine**
Thrust
Isp |
RD-107
223,000 lbf
991.7 kN
314 sec |
RD-108
224,100 lbf
997.1 kN
315 sec |
RD-461
67,000 lbf
298.2 kN
330 sec |
11D-53
15,000 lbf
66,700 N
340 sec |
| Number of Engines |
1 (per strap-on) |
1 |
1 |
1 |
| Nominal Burn Time |
118 sec |
286 sec |
230 - 250 sec |
192 sec |
** Note: Vacuum engine performance unless
otherwise specified.
|
