On methods of parameters determination of aviation missiles separation, during ground testing of aviation ejection launchers

Аuthors

Pravidlo M. N., Daneko A. I.

Toropov Machine-Building Design Bureau "Vimpel", 90, Volokolamskoe shosse, Moscow, 125424, Russia

Abstract

In this article are discussed methods of conducting test bench (ground) testing of aviation ejection launchers and experimental data evaluation, allowing getting required parameters with greater precision for required parameters and characteristics for correcting mathematical models of these units.

Keywords:

aircraft-carrier, aviation guided missile, mathematical modeling of separation dynamics, aviation ejection launcher, separation parameters, test bench (ground) testing, high-frequency g-load sensors