A breakdown surface model for thermal backscattering from the exhaust plume of a space-based HF laser
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Author
Contributions
- Naval Postgraduate School (U.S.) - Contributor
Publication
1986 - Naval Postgraduate School, Monterey, California, California
Language
English
Word Count
10,250 words, Guess
Page Count
41 pages
Identifiers
- Internet Archivebreakdownsurface00falc
- OCLC Control Number85177029
- Open LibraryOL25511237M
Alternate Titles
- NPS-67-86-002CR.
Description
The purpose of this report is to present a breakdown surface model for evaluating thermal backscattering flow from the supersonic exhaust plume of a gaseous mixture of H, HF, H2, DF and He. Fluxes of these species are considered separately. The model is carefully analyzed and is shown to overestimate the flux. Actual flux levels of the heavy corrosive molecules (HD, DF) have been found to be exceedingly low. It is concluded that the contribution of thermal backscattering to contaminating flux of HF and DF can be neglected.
Subjects
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