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 |
Strela
(RS-18) |
3,750 lbm
1,700 kg |
US
$10.5 M |
Two Stage Storable
Propellant |
229,000 lbm
104,000 kg |
* Performance provided by
AIAA, "International Reference Guide to Space Launch
Systems", 3rd edition.
Vehicle Configuration
| |
Stage 1 |
Stage 2 |
| Length |
56.4 ft
17.2 m |
12.8 ft
3.9 m |
| Diameter |
8.2 ft
2.5 m |
8.2 ft
2.5 m |
| Gross Mass |
|
|
Propellant
Propellant Mass |
N2O4 / UDMH
~175,000 lbm
80,000 kg |
N2O4 / UDMH
30,000 lbm
14,000 kg |
Engine
Thrust (vacuum)
Isp (vacuum) |
RD-0233
420,400 lbf
1870 kN
310 sec |
RD-035
54,000 lbf
240,000 N
320 sec |
| Number of Engines |
4 |
1 |
| Nominal Burn Time |
121 sec |
183 sec |
|
