R-36M2 (15A18M; Voevoda)
|
R-36M2 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-274 |
4 x 1 |
4,594.8 |
2901 |
4,950.5 |
3125 |
UDMH/N2O4 |
150.20 |
~95 |
1.5840 |
469.4 |
|
|
2 |
RD-0256 |
1 |
|
|
836.5 |
3334 |
UDMH/N2O4 |
37.60 |
~150 |
0.2509 |
125.4 |
|
|
RD-0257 |
4 |
|
|
? |
? |
? |
||||||
|
PBV |
RD-869 |
mod |
4 |
20.21 | 3069 |
UDMH/N2O4 |
0.0066 | |||||
| mod | 8.28 | 2964 | 0.0028 | |||||||||
15D285 (RD-274)
