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Saturn MLV-V-4(S)-A
Part of Saturn V
Saturn V 120
Saturn V 120" SRB
Saturn V 120 inch strapons
Credit: © Mark Wade
American orbital launch vehicle. MSFC study, 1965. 4 Titan UA1205 solid rocket boosters; Saturn IC stretched 337 inches with 6.0 million pounds propellant and 5 F-1 engines; S-II with 970,000 pounds propellant and 5 J-2 engines; S-IVB strengthened but with standard 230,000 lbs propellant, 1 J-2 engine.

Status: Study 1965. Payload: 160,880 kg (354,670 lb). Thrust: 54,920.00 kN (12,346,500 lbf). Gross mass: 4,615,440 kg (10,175,300 lb). Height: 113.00 m (370.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 160,880 kg (354,670 lb) to a 185 km orbit at 28.00 degrees. Payload: 57,500 kg (126,700 lb) to a translunar trajectory. Flyaway Unit Cost 1985$: 71.920 million.

Stage Data - Saturn MLV-V-4(S)-A



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: F-1. Stages: Saturn MS-II-1, Saturn MS-IVB-1, Saturn MS-IC-4(S)B, UA1205.

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