|
Propulsion Juno II
|
Rocketdyne S-3D
|
LR-79-NA-1 (S-3D)
|
|
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. S-3D
|
667.2 |
2432 |
758.7 |
2766 |
49.90 |
181.8 |
0.2745 |
138.0 |
| 2 |
Sergeant (11)
|
|
|
73.4 |
2158 |
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 |
|
