Analysis of Falling Attitude Based on Vertical Cold Launch Missile's Failure to Ignite
YANG Ming
LIU Bingjie
ZHANG Lei
JI Haiyan
Abstract：There is a possibility of ignition failure for ship borne missiles using cold ejection ignition.If the missile falls back onto the launch platform,there is a risk of platform deformation or even engine fire.This article applies ADAMS software to conduct dynamic simulation of the ejection drop process of a missile with failed cold ejection ignition,analyzes the changes in the attitude of the missile during the drop process,and provides theoretical support for subsequent research on missile drop safety.
Keywords：missilefallingdynamic simulationattitude
Publication Date：2025-04-20
Online Publishing Date：2025-08-15(First online date of this platform, not the publication date of the document)
Pages：4( 38-40,66 )