Propulsion Redstone-Sparta
|
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 |
||
| 1 |
NAA75-110-A6 |
311.4 | 1917 | 359.9 | 2216 | 19.67 | 121 | 0.1624 | 43.6 |
| 2 |
Antares II |
93.2 | 2579 | 1.37 | 38 | 0.0361 | 3.5 | ||
| 3 |
Alcyone |
27.4 | 2677 | 0.087 | 8.4 | 0.0103 | 0.2 |