This page no longer updated from 31 October 2001.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

Family: Winged. Country: USA. Status: Study 1962.

Early two-stage-to-orbit shuttle study, using storable propellants, Dynasoar-configuration delta wing orbiter and booster.


Liftoff Thrust: 1,320,820 kgf. Total Mass: 1,133,786 kg. Core Diameter: 7.0 m. Total Length: 78.0 m. Flyaway Unit Cost $: 36.00 million. in 1985 unit dollars.


Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .