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Instrumentation for near-Earth measurement of orbital debris and cosmic dust particlesDust instrumentation based on polyvinylidene fluoride (PVDF) dust sensor arrays is described which will measure the masses, fluxes, velocities, and trajectories of orbital debris particles and natural micrometeoroids. Orbital debris particles are distinguished from natural particles (cosmic dust) by means of the velocity/trajectory information. The instrumentation will measure particle trajectory with a mean error of approximately 7 degrees (for isotropic flux) and is designed for measurements over the particle diameter range of approximately 2 to 200 micro-m. For future missions having Earth-return capabilities, arrays of capture cell devices positioned behind the PVDF trajectory system would provide for Earth-based chemical and isotopic analysis of captured dust.
Document ID
19920018085
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tuzzolino, Anthony J.
(Chicago Univ. Chicago, IL, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1992
Publication Information
Publication: NASA. Langley Research Center, Second LDEF Post-Retrieval Symposium Abstracts
Subject Category
Instrumentation And Photography
Accession Number
92N27328
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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