This page no longer updated from 31 October 2001.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

Family: VTOVL. Country: USA. Status: Study 1969.

Boeing study, 1969, for Saturn follow-on. Plug nozzle, single-stage-to-orbit launch vehicle could itself put 1 million pounds payload into orbit. By addition of up to 12 260 inch solid motors up to 3.5 million pounds payload into orbit with a single launch.


Liftoff Thrust: 31,980,770 kgf. Total Mass: 25,132,660 kg. Core Diameter: 21.9 m. Total Length: 94.0 m. Flyaway Unit Cost $: 1,339.80 million. in 1985 unit dollars.


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Last update 12 March 2001.
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