Saturn V
Country of Origin: United States
Manufacturer: Boeing, North American, Douglas
Height: 110.6 m
Diameter: 10.1 m
Payload to LEO: 140 tons
Total Mass: 2970 tons
Launch Sites: Cape Canaveral
First Flight: November 9, 1967
Last Flight: May 14, 1973
Total Launches: 13
Successful Launches: 12
Saturn V
| Stage | Diameter | Fuel | Engine | Time | Thrust (Vac.) | ISP (SL / Vac.) | Mass / Empty Mass |
|---|---|---|---|---|---|---|---|
| 1 (S-IC) | 10.1 m | RP-1 / LOX | 5 x F-1 | 165 s | 5 x 7770 kN | 263 s / 304 s | 2290 tons / 287 tons |
| 2 (S-II) | 10.1 m | LH2 / LOX | 5 x J-2 | 360 s | 5 x 1033 kN | ? / 421 s | 496.2 tons / 88.4 tons |
| 3 (S-IVB) | 6.6 m | LH2 / LOX | J-2 | 500 s | 1033 kN | ? / 421 s | 123 tons / 13.5 tons |
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