Emission Properties and Stability of Internal Air Launch System

Abstract

Aiming at the characteristics of complex structure, changeable movement and the difference in emission and stability, put forward the emission performance index based on the study of internal air launch system; study the influence of the initial pitch angle of the carrier, characteristic diameter of stabilization parachute and some other characteristic parameters on emission properties; study the system's stability and put forward the concept of generalized stability through the research of kinetic equation, moreover, calculate stability domain through Monte Carlo calculation method.