Derivation Of Theoretical Calculations Of The Acoustic Problem With Experimental Data

Abstract

This work presents the results of complex experimental and computational studies of the shock-wave and thermodynamic parameters of the collision of a particle with the wall of the pressurized compartment of a spacecraft, depending on the physical and mechanical characteristics of the impactor material and the impact velocity. The results of calculations of the parameters of the wall breakdown and air waves in the pressurized compartment of the spacecraft are compared with the data of experimental measurements.