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Saturn V-D
Part of Saturn V
Saturn V 260
Saturn V 260" SRB
Saturn V 260 inch strapons
Credit: © Mark Wade
American orbital launch vehicle. MSFC study, 1968. Rehashed the Boeing 1967 studies, covering a variety of stage stretches and 120, 156, or 260 inch solid rocket boosters, but with S-ID stage-and-a-half first stage.

Status: Study 1968. Payload: 326,500 kg (719,800 lb). Thrust: 161,846.50 kN (36,384,541 lbf). Gross mass: 9,882,100 kg (21,786,300 lb). Height: 102.00 m (334.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 326,500 kg (719,800 lb) to a 185 km orbit at 28.00 degrees. Payload: 112,000 kg (246,000 lb) to a translunar trajectory. Flyaway Unit Cost 1985$: 736.600 million.

Stage Data - Saturn V-D



Family: orbital launch vehicle. People: von Braun. Country: USA. Stages: Saturn II, AJ-260X, Saturn IVB (S-V), Saturn S-ID Booster, Saturn S-ID Sustainer.
Photo Gallery

Saturn II stageSaturn II stage
Credit: © Mark Wade



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