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Modular space structuresThe Extendable Tetrahedral Truss orbiting antenna concept, comprising the use of prefabricated, automatically deployable lattice structures and their subsequent assembly into larger structures suitable for microwave antenna use, is described. It is assumed that the Space Shuttle Orbiter payload bay will be able to accommodate only modular portions of the structural system required, and that the Space Shuttle crew will furnish the manual labor entailed by orbital assembly. It is concluded that a deployable beam module system may be a more elegant design solution than the alternative triangular-module system.
Document ID
19810046987
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vaughan, D. H.
(General Dynamics Corp. Convair Div., San Diego, Calif., United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1980
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
SAWE PAPER 1371
Meeting Information
Meeting: Annual Conference of the Society of Allied Weight Engineers
Location: St. Louis, MO
Start Date: May 12, 1980
End Date: May 14, 1980
Sponsors: Society of Allied Weight Engineers
Accession Number
81A31391
Distribution Limits
Public
Copyright
Other

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