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Method of Fabricating NASA-Standard Macro-Fiber Composite Piezoelectric ActuatorsThe NASA Macro-Fiber Composite actuator is a flexible piezoelectric composite device designed for controlling vibrations and shape deformations in high performance aerospace structures. A complete method for fabricating the standard NASA Macro-Fiber Composite actuator is presented in this document. When followed precisely, these procedures will yield devices with electromechanical properties identical to the standard actuator manufactured by NASA Langley Research Center.
Document ID
20030063125
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
High, James W.
(NASA Langley Research Center Hampton, VA, United States)
Wilkie, W. Keats
(Army Research Lab. Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2003
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:212427
ARL-TR-2833
NASA/TM-2003-212427
L-18237
Report Number: NAS 1.15:212427
Report Number: ARL-TR-2833
Report Number: NASA/TM-2003-212427
Report Number: L-18237
Funding Number(s)
OTHER: 755-06-00-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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