This page no longer updated from 31 October 2001. Latest version can be found at Juno V-B

Family: Saturn C. Country: USA. Status: Study 1958.

A proposed version of the Juno V for lunar and planetary missions used a Titan I ICBM first stage and a Centaur high-energy third stage atop the basic Juno V cluster. Masses, payload estimated.


LEO Payload: 12,500 kg. to: 185 km Orbit. at: 28.0 degrees. Payload: 3,500 kg. to a: Translunar trajectory. Liftoff Thrust: 682,200 kgf. Total Mass: 539,480 kg. Core Diameter: 6.5 m. Total Length: 60.0 m. Flyaway Unit Cost $: 73.80 million. in 1985 unit dollars.


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Last update 12 March 2001.
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© Mark Wade, 2001 .