The supermodule - A design departure from the Shuttle payload paradigmAn effort has been made to formulate a novel approach to the construction of manned orbital facilities, in the context of a long-term launch strategy. The pressurized volume component of a manned platform is the point of departure, and an integrated vehicle designated the 'Supermodule' is defined which replaces analogous Space Station Freedom pressurized volume components. A launch sequence encompassing one Supermodule, one Shuttle Orbiter, and three Shuttle-Derived Vehicle cargo launchers, could reduce the number of launches needed to build a Space Station of the size of Freedom from 20 to merely five.
Document ID
19900040589
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murbach, Marcus S. (NASA Ames Research Center Moffett Field, CA, United States)
Garin, Vladimir M. (Bionetics, Inc. Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AIAA PAPER 90-0716Report Number: AIAA PAPER 90-0716