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An inadvertent capture cell for orbital debris and micrometeorites - The main electronics box thermal blanket of the solar maximum satelliteThe physical properties of impact features in the Solar Max main electronics box thermal blanket are consistent with hypervelocity impacts of particles in the near-earth space environment. The majority of particles are orbital debris and include spacecraft paints and bismuth-rich particles. At least 30 percent of all impact features are caused by micrometeorites, which include silicates and sulfides. Some micrometeorites survive impact with only minor shock-metamorphic effects or chemical fractionation. Currently calibration experiments are under way to relate flux to particle diameter (or mass).
Document ID
19870057123
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Rietmeijer, F. J. M.
(Lockheed Engineering and Management Services Co., Inc. Houston, TX, United States)
Schramm, L. S.
(Lockheed Engineering and Management Services Co., Inc. Houston, TX, United States)
Barrett, R. A.
(Lockheed Engineering and Management Services Co., Inc. Houston, TX, United States)
Mckay, D. S.
(Lockheed Engineering and Management Services Co., Inc. Houston, TX, United States)
Zook, H. A.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1986
Publication Information
Publication: Advances in Space Research
Volume: 6
Issue: 7 19
ISSN: 0273-1177
Subject Category
Spacecraft Instrumentation
Accession Number
87A44397
Funding Number(s)
CONTRACT_GRANT: NASA TASK 152-17-40-20
CONTRACT_GRANT: NASA TASK 906-75
Distribution Limits
Public
Copyright
Other

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