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.
To achieve orbit, the
launch vehicle is equipped with a solid kick motor. Satellite
payloads are accommodated in a protected capsule mounted in the
warhead section of the SLBM.
| |
LEO Payload
(70-80°, 600 km) |
LEO Payload
(52°, 900 km) |
Configuration |
Launch Mass |
Volna
(R-29R)
Barents Sea |
110 lbm
50 kg |
N/A |
Three
Stage |
77,801
lbm
35,300 kg |
Volna
(R-29R)
Pacific Ocean |
N/A |
110 lbm
50 kg |
Three
Stage |
77,801
lbm
35,300 kg |
Vehicle Configuration
| |
Stage 1 |
Stage 2 |
Stage
3 |
| Length |
|
|
|
| Diameter |
5.9 ft
1.8 m |
|
|
| Gross Mass |
|
|
|
Propellant
Propellant Mass |
N2O4 / UDMH
? lbm
? kg |
N2O4 / UDMH
? lbm
? kg |
Solid
? lbm
? kg |
Engine
Thrust (vacuum)
Isp (vacuum) |
|
|
|
| Number of Engines |
|
|
|
| Nominal Burn Time |
|
|
|
|
