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| Propulsion ABL RS-1 |
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|
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 |
Comb. |
tons |
s |
t/s |
MN*s |
||
| - | E2 (1) | 58.13 | 2824 | 65.79 | 3197 |
|
0.0206 |
- | ||
| 1 |
E2 (9) |
523.1 | 2824 |
592.2 |
3197 |
Kerosene/LOX | 29.64 |
160 |
0.1852 |
94.7 |
|
2 |
E2 Vac |
66.59 | 3236 | 7.1 | 345 | 0.0206 | 23.0 | |||
