Complex analysis of launch and separation system of aviation guided missiles

Аuthors

Pravidlo M. N.

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

Abstract

In this article are substantiated complex approach to design system for launch and separation aviation guided missiles from aircraft-carrier by aviation launcher and aviation ejection launcher. Results are provided for analysis of aircraft-carrier, launcher and missile influence on ensuring safety of missiles separation. Ways are showed for solving problem of ensuring safety of aviation guided missile separation from aircraft-carrier.

Keywords:

aircraft-carrier, aviation guided missile, aviation launcher, aviation ejection launcher, separation parameters, separation safety, launch and separation system.