Propulsion Chang Zheng
9 |
Engines |
Propulsion |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Flow rate |
|
|
Chambers |
kN |
N*s/kg |
kN |
N*s/kg |
t/s |
|
YF-130 (4) |
2 | Kerosene/LOX | 16,970.7 | 3001 | 18,828.6 | 3329 | 5.6554 |
YF-90 (2) |
1 |
LH2/LOX |
- | - | 4,413.0 | 4538 | 0.9726 |
YF-79 (4) |
1 | - | - | 972.7 | 4511 | 0.2156 |