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The S-IC (pronounced S-one-C) was the first stage of the American Saturn V rocket. The S-IC stage was manufactured by the Boeing Company. Like the first stages of most rockets, more than 90% of the mass at launch was propellant, in this case RP-1 rocket fuel and liquid oxygen (LOX) oxidizer. It was 42 m (138 ft) tall and 10 m (33 ft) in diameter. The…
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stage saturn engines f-1 tank first five stages thrust rocket boeing study fuel flight engine propellant 000 intended liquid oxygen
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| S-IC | Burn time | 150 seconds | 1.00 | infobox |
| S-IC | Country of origin | United States | 1.00 | infobox |
| S-IC | Diameter | 10 m (33 ft) | 1.00 | infobox |
| S-IC | Empty mass | 137 t (303,000 lb) | 1.00 | infobox |
| S-IC | First flight | November 9, 1967 (Apollo 4) | 1.00 | infobox |
| S-IC | Gross mass | 2,214 t (4,881,000 lb) | 1.00 | infobox |
| S-IC | Height | 42 m (138 ft) | 1.00 | infobox |
| S-IC | Last flight | May 14, 1973 (Skylab 1) | 1.00 | infobox |
| S-IC | Manufacturer | Boeing | 1.00 | infobox |
| S-IC | Maximum thrust | 34,500 kN (7,750,000 lbf) at sea level | 1.00 | infobox |
| S-IC | Powered by | 5 × F-1 | 1.00 | infobox |
| S-IC | Propellant | RP-1/LOX | 1.00 | infobox |
| S-IC | Propellant mass | 2,077 t (4,578,000 lb) | 1.00 | infobox |
| S-IC | Specific impulse | 263 s (2.58 km/s) | 1.00 | infobox |
| S-IC | Status | Retired | 1.00 | infobox |
| S-IC | Successes (stage only) | 13 | 1.00 | infobox |
| S-IC | Total launches | 13 | 1.00 | infobox |
| S-IC | Used on | Saturn V | 1.00 | infobox |
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