| UR-200 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-0203/-0204 |
3 + 1 | 1,998.4 | 2726 | 2,235.5 | 3050 |
UDMH/N2O4 |
0.7330 |
|
||
| 2 |
RD-0206 |
1 | 575.6 | 3197 |
UDMH/N2O4 |
0.1800 | |||||
| RD-0207 | 4 | 30.4 | 2912 | 0.0104 | |||||||
