Propulsion Saturn
V
Saturn V (Apollo 11)
Stage
|
Engines
|
Sequence
|
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 |
F-1 (5)
|
1 |
34,478.2 |
2550 |
40,312.9 |
2981 |
1,920.18 |
142 |
13.5224 |
6,401.7 |
F-1 (4)
|
2 |
27,582.5 |
2550 |
32,250.0 |
2981 |
227.09 |
21 |
10.8178 |
2 |
J-2 (5)
|
1 |
|
|
5,004.3 |
4171 |
6.00 |
5 |
1.1999 |
1,849.3 |
J-2 (5)
|
2 |
|
|
5,160.0 |
4161 |
362.08 |
292 |
1.2401 |
J-2 (4)
|
3 |
|
|
3,505.2 |
4173 |
76.10 |
90.6 |
0.8400 |
3 |
J-2
|
|
|
|
876.3 |
4173 |
106.83 |
508.7 |
0.2100 |
445.8 |
Saturn V (Apollo 17)
Stage
|
Engines
|
Sequence
|
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 |
F-1 (5)
|
1 |
34,478.2 |
2550 |
40,312.9 |
2981 |
1,920.18 |
142 |
13.5224 |
6,466.2 |
F-1 (4)
|
2 |
27,582.5 |
2550 |
32,250.0 |
2981 |
249.11 |
23 |
10.8178 |
2 |
J-2 (5)
|
1 |
|
|
5,004.3 |
4171 |
6.00 |
5 |
1.1999 |
1,881.2 |
J-2 (5)
|
2 |
|
|
5,160.0 |
4161 |
362.08 |
292 |
1.2401 |
J-2 (4)
|
3 |
|
|
3,505.2 |
4173 |
83.75 |
99.7 |
0.8400 |
3 |
J-2
|
|
|
|
876.3 |
4173 |
108.11 |
514.8 |
0.2100 |
451.1 |
Saturn V (Skylab)
Stage
|
Engines
|
Sequence
|
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 |
F-1 (5)
|
1 |
34,478.2 |
2550 |
40,312.9 |
2981 |
1,920.18 |
142 |
13.5224 |
6,301.7 |
F-1 (4)
|
2 |
27,582.5 |
2550 |
32,250.0 |
2981 |
194.16 |
17.9 |
10.8178 |
2 |
J-2 (5)
|
1 |
|
|
5,004.3 |
4171 |
6.00 |
5 |
1.1999 |
1,975.9 |
J-2 (5)
|
2 |
|
|
5,160.0 |
4161 |
362.08 |
292 |
1.2401 |
J-2 (4)
|
3 |
|
|
3,505.2 |
4173 |
106.43 |
126.7 |
0.8400 |
SM engine AJ-10-137
|
TRW LMDE
|
LMAE RS-18
|
|