R-36MU (15A18; Satan)
Dnepr (right) is a R-36MU with R-36M2 upper stage
and PBV/fairing change
| R-36MU ICBM | Thrust s.l. | Isp s.l. | Thrust vac | Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp.(vac) |
||||
| Stage |
Engines |
Chamb. |
kN | Ns/kg | kN | Ns/kg |
Fuel/Oxidizer |
tons |
sec |
t/sec |
MN*sec |
|
| 1 |
RD-264 |
4 x 1 | 4,166.3 | 2876 | 4,522.8 | 3122 |
UDMH/N2O4 |
147.90 | ~102 | 1.4485 |
461.8 |
|
| 2 |
RD-0229 |
1 | 760.0 | 3334 |
UDMH/N2O4 |
36.75 | ~161 | 0.2279 | 122.5 | |||
| RD-0230 | 4 | ? | ? | ? | ||||||||
| PBV |
RD-869 |
mod | 4 | 20.21 | 3069 |
UDMH/N2O4 |
0.0066 | |||||
| mod | 8.28 | 2964 | 0.0028 | |||||||||
