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 |
|
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 |