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Saturn C-3B
Part of Saturn V
Saturn C-33B 3 Stage
Saturn C-33B 3 Stage
Saturn C-33B 3 Stage version Nov 1961
Credit: © Mark Wade
American orbital launch vehicle. Final configuration of the Saturn C-3 at the time of selection of the Saturn C-5 configuration for the Apollo program in December 1961.

Status: Study 1961. Payload: 78,000 kg (171,000 lb). Thrust: 20,010.00 kN (4,498,420 lbf). Gross mass: 1,690,590 kg (3,727,110 lb). Height: 85.00 m (278.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 78,000 kg (171,000 lb) to a 185 km orbit at 28.00 degrees. Payload: 25,000 kg (55,000 lb) to a translunar trajectory.

Stage Data - Saturn C-3B



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: F-1, J-2. Stages: Saturn IC C-3B, Saturn II C-5A, Saturn IVB C-3B.
Photo Gallery

Saturn A-1 to C-5Saturn A-1 to C-5
Credit: © Mark Wade


Saturn C-3B finalSaturn C-3B final
Saturn C-3B final configuration Nov 1961
Credit: © Mark Wade


Saturn C-3B 2 Stage Saturn C-3B 2 Stage
Saturn C-3B 2 Stage version Nov 1961
Credit: © Mark Wade



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