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Saturn MLV-V-1A
Part of Saturn V
American orbital launch vehicle. MSFC study, 1965. Saturn IC stretched 240 inches with 5.6 million pounds propellant and 6 F-1 engines; S-II stretched 156 inches with 1.2 million pounds propellant and 7 J-2 engines; S-IVB stretched 198 inches with 350,000 lbs propellant, 1 J-2 engine.

Status: Study 1965. Payload: 145,000 kg (319,000 lb). Thrust: 40,485.10 kN (9,101,413 lbf). Gross mass: 3,648,700 kg (8,044,000 lb). Height: 121.00 m (396.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 145,000 kg (319,000 lb) to a 185 km orbit at 28.00 degrees. Payload: 54,400 kg (119,900 lb) to a translunar trajectory.

Stage Data - Saturn MLV-V-1A



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: F-1. Stages: Saturn MS-IC-1A, Saturn MS-II-1A, Saturn MS-IVB-1A.

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