Saturn I and IB
Country of Origin: United States
Manufacturer: Chrysler, Douglas
Height: 55 m
Diameter: 6.6 m
Payload to LEO: 20 to 21 tons
Total Mass: 1124 to 1300 tons
Launch Sites: Cape Canaveral
First Flight: October 27, 1961 (Saturn I); February 26, 1966 (Saturn IB)
Last Flight: July 30, 1965 (Saturn I); July 15, 1975 (Saturn IB)
Total Launches: 10 (Saturn I); 9 (Saturn IB)
Successful Launches: 10 (Saturn I); 9 (Saturn IB)
Saturn I
| Stage | Diameter | Fuel | Engine | Time | Thrust (Vac.) | ISP (SL / Vac.) | Mass / Empty Mass |
|---|---|---|---|---|---|---|---|
| 1 (S-I) | 6.52 m | RP-1 / LOX | 8 x H-1 | 150 s | 8 x 1020 kN | 255 s / 289 s | |
| 2 (S-IV) | LH2 / LOX | 6 x RL10 | 482 s | 6 x 65.6 kN | ? / 444 s | ||
| 3 (S-V) (Centaur-C) (unflown) | LH2 / LOX | 2 x RL10 | 430 s | 2 x 65.6 kN | ? / 444 s |
Saturn IB
| Stage | Diameter | Fuel | Engine | Time | Thrust (Vac.) | ISP (SL / Vac.) | Mass / Empty Mass |
|---|---|---|---|---|---|---|---|
| 1 (S-IB) | 6.61 m | RP-1 / LOX | 8 x H-1 | 150 s | 8 x 1020 kN | 255 s / 289 s | |
| 2 (S-IVB-200) | LH2 / LOX | J-2 200lbf | 480 s | 890 kN | ? / 421 s |
Links:
Destination Orbite – Saturn IB
Space Launch Report – Saturn I
Space Launch Report – Saturn IB