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Spacecraft recontaminationA computer simulation program to model the redistribution of particulate contaminants on a spacecraft after launch was developed. The component models for particulate adhesion, meteoroid impact, and electrostatic forces are described and intermediate results are presented. The results of a sample calculation show that the recontamination process is important.
Document ID
19760004027
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barengoltz, J. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Edgars, D. (Bionetic Corp.)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: NASA. Goddard Space Flight Center 8th Conf. on Space Simulation
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
PAPER-2
Accession Number
76N11115
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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