Template:Saturn IB infobox
From Wikipedia, the free encyclopedia
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| Fact sheet | |
|---|---|
| Size | |
| Height | 68.3 m (224 ft) |
| Diameter | 6.6 m (21.7 ft) |
| Mass | 600,795 kg (1,300,000 lb) |
| Stages | 2 |
| Capacity | |
| Payload to LEO | 18,600 kg |
| First Stage - S-IB | |
| Engines | 8 F-1 engines |
| Thrust | 7.6 MN (1,700,000 lbf) |
| Burn time | 150 s |
| Fuel | RP-1 and liquid oxygen |
| Second Stage - S-IVB | |
| Engines | 1 J-2 engine |
| Thrust | 1 MN (225,000 lbf) |
| Burn time | 470 s |
| Fuel | Liquid hydrogen and liquid oxygen |
