Engines Redstone & Juno I
Juno I
|
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 | Rock. A-7 | 369.0 | 2305 | 416.2 | 2599 | 24.80 | 155 | 0.1600 | 64.5 |
| 2 | Sergeant (11) | 73.4 | 2157 | 0.237 | 6.5 | 0.035 | 0.51 | ||
| 3 | Sergeant (3) | 24.0 | 2305 | 0.066 | 7 | 0.010 | 0.15 | ||
| 4 | Sergeant (1) | 8.0 | 2305 | 0.022 | 7 | 0.003 | 0.05 |
Redstone-Mercury
|
Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
| - | - | kN | Ns/kg | kN | Ns/kg | tons | s | t/s | MN*s |
| 1 | Rock. A-7 | 369.0 | 2305 | 416.2 | 2599 | 22.90 | 143 | 0.1600 | 59.5 |