|
Propulsion ex Soyuz-5
|
RD-0164
|
?
RD-0169
|
RD-0124M
|
ex Soyuz-5 (Methane)
|
Stage
|
Engines
|
Thrust s.l.
|
Isp s.l.
|
Thrust vac
|
Isp vac
|
Propellant
|
Burn time
|
Flow rate
|
Total Imp
|
|
kN
|
N*s/kg
|
kN
|
N*s/kg
|
tons
|
s
|
t/s
|
MN*s
|
|
Booster
(1)
|
RD-0164 (1)
|
3,334.2 |
3055 |
3,831.4 |
3511 |
184 |
168 |
1.0912 |
646.0 |
|
Core |
RD-0164 (1)
|
3,334.2 |
3055 |
3,831.4 |
3511 |
184 |
168 |
1.0912 |
646.0 |
|
2 |
RD-0169
|
|
|
715.9 |
3648 |
50 |
254 |
0.1962 |
182.4 |
|
3 |
RD-0124M (2)
|
|
|
49.1 |
3649 |
18.84 |
1400 |
0.0135 |
68.7 |
|
