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Experimental thermal mechanics of deployable boom structuresAn apparatus was developed for thermal distortion measurements on deployable boom structures. The calibration procedure and thermal static bending plus twist measurements are considered. The thermal mechanics test facility is described. A table is presented for several examples of spacecraft applications of thermal static distortion measurements on 3-m deployable booms.
Document ID
19720018139
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Predmore, R. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Publication Information
Publication: Significant Accomplishments in Technol., GSFC, 1970
Subject Category
Thermodynamics And Combustion
Accession Number
72N25789
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19720018105Collected WorksSignificant Accomplishments in Technology, Goddard Space Flight Center, 1970
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