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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
J Barengoltz (Jet Propulsion Laboratory Pasadena, United States)
D Edgars (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
N76-11115
Meeting Information
Meeting: Eight Conference on Space Simulation
Location: Silver Spring, MD
Country: US
Start Date: November 3, 1975
End Date: November 5, 1975
Sponsors: American Institute for Aeronautics & Astronautics, ASTM, National Aeronautics and Space Administration, American Society for Testing Materials
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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