DocumentCode
1357567
Title
Some effects of hypersonic ionization on the design of electrical and electronic components
Author
Sisco, W. B. ; Fiskin, J. M.
Author_Institution
Douglas Aircraft Company, Inc., Long Beach, Calif.
Volume
78
Issue
5
fYear
1959
Firstpage
352
Lastpage
356
Abstract
VEHICLES traveling at hypersonic velocities in a gaseous atmosphere will be surrounded by a shock-induced high-temperature sheath. As a result of the high temperature, the gaseous sheath has an electron density greater than that of the ambient atmosphere. Since the craft will be immersed in a high-temperature envelope, both it and its components will be subjected to unusual temperatures. Fig. 1 indicates the way in which the air temperature and density varies from the shock front to vehicle surface for a given velocity and altitude.
Keywords
Electric shock; Equations; Ionization; Plasma temperature; Power system reliability; Reliability; Vehicles;
fLanguage
English
Journal_Title
American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
Publisher
ieee
ISSN
0097-2185
Type
jour
DOI
10.1109/TAI.1959.6369063
Filename
6369063
Link To Document