Payload Performance
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
(?°, 200 km) |
Estimated Launch Price |
Configuration |
Launch Mass |
Shtil 1
(R-29RM) |
950 lbm
430 kg |
US
$100 - 300 k |
Three
Stage Storable
Propellant |
88,000 lbm
40,000 kg |
Shtil 2
(R-29RM) |
770 lbm
350 kg |
US
$100 - 300 k |
Three
Stage Storable
Propellant |
88,000 lbm
40,000 kg |
* Performance provided by
AIAA, "International Reference Guide to Space Launch
Systems", 3rd edition.
Vehicle Configuration
| |
Stage 1 |
Stage 2 |
Stage
3 |
| Length |
25 ft
7.7 m |
16 ft
4.9 m |
9.2 ft
2.8 m |
| Diameter |
6.2 ft
1.9 m |
6.2 ft
1.9 m |
6.2 ft
1.9 m |
| Gross Mass |
|
|
|
Propellant
Propellant Mass |
N2O4 / UDMH
? lbm
? kg |
N2O4 / UDMH
? lbm
? kg |
N2O4 / UDMH
? lbm
? kg |
Engine
Thrust (vacuum)
Isp (vacuum) |
RD-0233
153,000 lbf
682 kN
300 sec |
? |
? |
| Number of Engines |
1
main engine with 1 vernier with 4 thrusters |
? |
? |
| Nominal Burn Time |
Main
engine 74 sec
verniers 79 sec
|
? |
? |
|
