Saturn V 2

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Saturn V 2

Part of Saturn V

F-1 engine
Credit: © Mark Wade

American orbital launch vehicle. Two stage version of Saturn V, consisting of 1 x Saturn S-IC + 1 x Saturn S-II, used to launch Skylab.

First Launch: 1973-05-14. Last Launch: 1973-05-14. Number: 1 . Payload: 75,000 kg (165,000 lb). Thrust: 34,030.00 kN (7,650,240 lbf). Gross mass: 2,822,000 kg (6,221,000 lb). Height: 104.80 m (343.80 ft). Diameter: 10.06 m (33.00 ft). Apogee: 500 km (310 mi).

LEO Payload: 75,000 kg (165,000 lb).

More at: Saturn V 2.

Family: orbital launch vehicle. People: von Braun. Country: USA. Stages: Saturn IC, Saturn II, Saturn IVB (S-V).

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