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Structures that adapt to spaceIt is shown that by allowing adjustments in space, designs that incorporate adaptive structures can reduce initial precision requirements and lower costs. Present and future spacecraft structures will need enhancements in performance, reliability, testability, and cost-effectiveness; unless a structural system meets these demands, it probably will never be implemented operationally. Attention is given to the ASTREX test facility at Edwards AFB that includes embedded piezoelectric, in-line piezoelectric actuator, and magnetostrictive active members whose testbed rapidly slews the spacecraft through large angles and then points it quickly and accurately.
Document ID
19920072508
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Wada, Ben K.
(JPL Pasadena, CA, United States)
Tracy, John
(McDonnell Douglas Space Systems Co. Huntington Beach, CA, United States)
Date Acquired
August 15, 2013
Publication Date
September 1, 1992
Publication Information
Publication: Aerospace America
Volume: 30
Issue: 9, Se
ISSN: 0740-722X
Subject Category
Structural Mechanics
Report/Patent Number
ISSN: 0740-722X
Accession Number
92A55132
Distribution Limits
Public
Copyright
Other

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