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Saturn INT-27
Part of Saturn I
Saturn IB-INT-27
Saturn IB-INT-27
Credit: © Mark Wade
American orbital launch vehicle. UA study, 1965. Saturn variant using various combinations of 156 inch rocket motors as first and second stages, with S-IVB upper stage.

Status: Study 1965. Payload: 40,000 kg (88,000 lb). Thrust: 65,813.00 kN (14,795,350 lbf). Gross mass: 3,068,800 kg (6,765,500 lb). Height: 67.00 m (219.00 ft). Diameter: 6.61 m (21.68 ft). Apogee: 185 km (114 mi).

Number of Strapon Motors4322
Number of Core Stage Motors1110
Payload with 4 Segment Motors79,00068,00054,00036,000
Payload with 3 Segment Motors70,00059,00045,00029,000
Payload with 2 Segment Motors57,00047,00036,00024,000
Payload with 1 Segment Motors45,00039,00027,00018,000

LEO Payload: 40,000 kg (88,000 lb) to a 185 km orbit at 28.00 degrees. Flyaway Unit Cost 1985$: 200.000 million.

Stage Data - Saturn INT-27



Family: orbital launch vehicle. People: von Braun. Country: USA. Stages: Saturn IVB (S-IB), UA-156.

1964 May 28 - . LV Family: Saturn I, Saturn V. Launch Vehicle: Saturn INT-27, Saturn V-25(S)B, Saturn V-25(S)U.

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