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NASA NTRS · 19760004027

Spacecraft recontamination

Abstract

A 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.

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BibTeXRIS

Barengoltz, J., Edgars, D.. 1975-01-01. Spacecraft recontamination. https://ntrs.nasa.gov/citations/19760004027

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