The effort reported on is part of a program to completely specify the susceptibility effects of the electromagnetic environment on weapon systems. Since the electromagnetic coupling into a system is dependent upon skin currents, the electrical properties and the effects of the exhaust plume must be completely determined. This report provides a mathematical description of the chemical and electrical characteristics of a typical tactical rocket. In particular the coaxial and radial distributions of the constitutive parameters in the wake of the rocket are developed from a plasma model of the exhaust plume. (Author)
A Plasma Model of Missile Exhaust Plumes. (Axial and Radial Conductivity Distributions for the Redeye Missile)
1977
134 pages
Report
Keine Angabe
Englisch
Surface Launched Missiles , Combustion & Ignition , Antiaircraft Defense Systems , Exhaust plumes , Electromagnetic compatibility , Plumes , Plasma medium , Surface to air missiles , Electromagnetic environments , Electromagnetic radiation , Rocket exhaust , Gas ionization , Computer programs , Predictions , Electrical properties , Wake , Chemical reactions , Thermodynamics , Antiaircraft ammunition , Redeye , Skin currents , Plasma electromagnetics
Preventing Aircraft Damage Due to Missile Exhaust Plumes
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