Roketatar yardımcı şase tasarımı ve doğrulanması

This thesis evaluates the structural suitability of the rocket launcher subframe under static and dynamic conditions with the help of finite element method. Rocket launchers generally fires rockets at stabilization position to have good rocket accuracy and dispersion performance so that the dynamic behaviour of subframe during firing will be examined. The subframe is also under various loads on off-road condition as a part of mission. In this thesis, the reliability of subframe and its components will be examined during firing and off-road conditions. The purpose of this thesis is to give tips for designing subframe, to analyse a finite element model and to verify the finite element model by taking the measurement in real test. Hence, to obtain a optimized rocket launcher subframe that can be integrated to tactical wheeled vehicle chassis is the key point of designing rocket launcher.