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Saturn V 2


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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). Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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