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Saturn V-ELV
Part of Saturn V
American orbital launch vehicle. NASA study, 1966. No-height-limitation stretched Saturn with Titan UA1207 motors for thrust augmentation.

Status: Study 1966. Payload: 200,000 kg (440,000 lb). Thrust: 59,392.70 kN (13,352,010 lbf). Gross mass: 5,172,820 kg (11,404,110 lb). Height: 124.00 m (406.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 200,000 kg (440,000 lb) to a 185 km orbit at 28.00 degrees. Payload: 67,000 kg (147,000 lb) to a translunar trajectory. Flyaway Unit Cost 1985$: 97.440 million.

Stage Data - Saturn V-ELV



Family: orbital launch vehicle. People: von Braun. Country: USA. Stages: Saturn MS-IC-4(S)B, Saturn MS-II-1A, Saturn MS-IVB-1A, UA1207.

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