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Space deployable truss structure designThe development status of the deployable box truss structure is summarized. Potential applications for this structural system are described. Structural and component design requirements derived from these applications are discussed. Components of prototype 4.6 m cubes which incorporate graphite/epoxy structural members, fittings, and mechanisms are described. The benefits of the component designs and their respective manufacturing processes are presented.
Document ID
19810013866
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Coyner, J. V., Jr. (Martin Marietta Aerospace Denver, CO, United States)
Tobey, W. H. (Martin Marietta Aerospace Denver, CO, United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1981
Publication Information
Publication: NASA. Marshall Space Flight Center The 15th Aerospace Mech. Symp.
Subject Category
Ground Support Systems And Facilities (Space)
Accession Number
81N22397
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19810013857Collected Works15th Aerospace Mechanisms Symposium
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