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Saturn IB-INT-27
Saturn IB-INT-27 -

Credit: © Mark Wade. 1,472 bytes. 74 x 386 pixels.

Family: Saturn I. Country: USA. Status: Study 1965.

UA study, 1965. Saturn variant using various combinations of 156 inch rocket motors as first and second stages, with S-IVB upper stage.

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. to: 185 km Orbit. at: 28.0 degrees. Liftoff Thrust: 6,711,060 kgf. Total Mass: 3,068,800 kg. Core Diameter: 6.6 m. Total Length: 67.0 m. Flyaway Unit Cost $: 200.00 million. in 1985 unit dollars.


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Last update 12 March 2001.
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