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Saturn A-2
Saturn A-2 -

Credit: © Mark Wade. 2,624 bytes. 76 x 661 pixels.

Family: Saturn C. Country: USA. Status: Study 1959.

More powerful version of Saturn I with low energy second stage consisting of cluster of four IRBM motors and tankage, Centaur third stage. Masses, payload estimated.


LEO Payload: 10,000 kg. to: 185 km Orbit. at: 38.0 degrees. Payload: 2,000 kg. to a: Translunar trajectory. Liftoff Thrust: 743,890 kgf. Total Mass: 702,960 kg. Core Diameter: 6.5 m. Total Length: 62.0 m. Flyaway Unit Cost $: 63.80 million. in 1985 unit dollars.


Saturn A-1 to C-5Saturn A-1 to C-5

Credit: © Mark Wade. 12,176 bytes. 639 x 461 pixels.

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Last update 12 March 2001.
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