NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Thermal expansion of composites: Methods and resultsThe factors controlling the dimensional stability of various components of large space structures were investigated. Cyclic, thermal and mechanical loading were identified as the primary controlling factors of the dimensional stability of cables. For organic matrix composites, such as graphite-epoxy, it was found that these factors include moisture desorption in the space environment, thermal expansion as the structure moves from the sunlight to shadow in its orbit, mechanical loading, and microyielding of the material caused by microcracking of the matrix material. The major focus was placed on the thermal expansion of composites and in particular the development and testing of a method for its measurement.
Document ID
19810010646
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bowles, D. E.
(NASA Langley Research Center Hampton, VA, United States)
Tenney, D. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
February 1, 1981
Publication Information
Publication: Large Space Systems Technol., 1980, Vol. 1
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
81N19173
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available