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.
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;
Journal_Title :
American Institute of Electrical Engineers, Part II: Applications and Industry, Transactions of the
DOI :
10.1109/TAI.1959.6369063