Propulsion Saturn
I & IB
Saturn I (Block 1)
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 |
H-1 (8)
|
1 |
5,871.7 |
2456 |
6,654.6 |
2783 |
264.23 |
110.5 |
2.3912 |
770.3 |
H-1 (4)
|
2 |
|
|
3,327.3 |
2783 |
12.55 |
10.5 |
1.1955 |
Saturn I (Block 2)
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
|
H-1 (8)
|
1
|
6,690.2
|
2525
|
7,473.1
|
2821
|
373.56
|
141
|
2.6490
|
1,076.1
|
H-1 (4)
|
2 |
|
|
3,736.5 |
2821 |
7.95 |
6 |
1.3245 |
2
|
RL-10A-3S (6)
|
|
|
|
400.3 |
4197 |
45.36 |
475.6 |
0.9538 |
190.4 |
Engine J-2
|
Saturn IB (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
|
H-1 (8)
|
1 |
7,117.2 |
2574 |
8,297.6 |
3001 |
389.86 |
141 |
2.7650 |
1,209.6 |
H-1 (4)
|
2 |
|
|
3,967.9 |
3001 |
13.82 |
10 |
1.3825 |
2
|
J-2
|
1 |
|
|
889.7 |
4187 |
1.06 |
5 |
0.2125 |
447.3 |
J-2
|
2 |
|
|
1,000.9 |
4168 |
70.08 |
292 |
0.2401 |
J-2
|
3
|
|
|
822.9 |
4217 |
35.69 |
183 |
0.1952 |
|