This page no longer updated from 31 October 2001. Latest version can be found at Starlifter

Family: Shuttle Proposals. Country: USA. Status: Study 1968.

Related to Lockheed Shuttle LS200 proposal. X-24B lifting body configuration orbiter with wrap-around drop tank.


Liftoff Thrust: 415,080 kgf. Total Mass: 300,408 kg. Core Diameter: 8.0 m. Total Length: 30.0 m. Flyaway Unit Cost $: 28.00 million. in 1985 unit dollars.


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