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A technique for position sensing and improved momentum evaluation of microparticle impacts in space.The design of a three element piezoelectric microparticle impact sensing diaphragm is described which is sensitive to the detection of momentum propagated by the bending wave. The design achieves a sensitivity of .03 microdyn/sec and optimizes the detection of the direct-path pulse from impact relative to secondary reflections and interference from discontinuities. Measurement of the relative arrival times and the maximum amplitudes of the outputs from the three piezoelectric sensors leads to the determination of the impact position and the normally resolved impact momentum exchange. Coincidence of the signals and a partial redundancy of data leads to a very high noise discrimination.
Document ID
19720053852
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Mcdonnell, J. A. M.
(Kent, University, Canterbury, Kent, England; NASA, Goddard Space Flight Center Greenbelt, Md., United States)
Abellanas, C.
(Kent, University Canterbury, Kent, United Kingdom)
Date Acquired
August 6, 2013
Publication Date
August 1, 1972
Publication Information
Publication: Review of Scientific Instruments
Volume: 43
Subject Category
Instrumentation And Photography
Accession Number
72A37518
Funding Number(s)
CONTRACT_GRANT: SRC-SG-S-181
CONTRACT_GRANT: SRC-B-SR-8718
Distribution Limits
Public
Copyright
Other

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