Title of article :
Combat stiffness of the launcher platform
Author/Authors :
Lazarevic ، Miloš S. Faculty of Engineering - University of Kragujevac
From page :
904
To page :
923
Abstract :
Possible loads on a multiple rocket launcher have been systemized and analyzed. Based on the analysis of loads, a mathematical-mechanical model has been made to describe the stability of a MLR hit by a high explosive-fragmentation projectile (HE-FRAG) in a close range. The results give the dependency of the launcher stability on explosion proximity, its type and the explosive charge mass. The stability limit is determined by the force that can turn over the laucher and compromise the stability of projectiles inside. To simplify the given model, the kinetic energy is calculated for a projectile fragment that hits the launcher.
Keywords :
load , explosion effect , surface explosion , above ground explosion , conditions , critical pressure , critical distance , overturn , stability , kinetic energy ,
Journal title :
Military Technical Courier
Journal title :
Military Technical Courier
Record number :
2508967
Link To Document :
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