Current spacecraft implement relatively uncoupled material and
structural systems to address a variety of design requirements,
including structural integrity, damage tolerance, radiation
protection, debris shielding and thermal insulation. This
investigation provided an initial assessment of multi-functional
sandwich composites to integrate these diverse requirements. The
need for radiation shielding was addressed through the selection of
polymeric constituents with high hydrogen content. To provide
increased damage tolerance and debris shielding, manufacturing
techniques were developed to incorporate transverse stitching
reinforcement, internal layers, and a self-healing ionomer
membrane. To assess the effects of a space environment, thermal
expansion behavior of the candidate foam materials was investigated
under a vacuum and increasing temperature. Finally, a thermal
expansion model was developed for foam under vacuum conditions and
its predictive capability assessed.
General
Imprint: |
Bibliogov
|
Country of origin: |
United States |
Release date: |
July 2013 |
First published: |
July 2013 |
Authors: |
Daniel O. Adams
|
Dimensions: |
246 x 189 x 10mm (L x W x T) |
Format: |
Paperback - Trade
|
Pages: |
188 |
ISBN-13: |
978-1-289-23741-7 |
Categories: |
Books >
Social sciences >
Politics & government >
General
|
LSN: |
1-289-23741-7 |
Barcode: |
9781289237417 |
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