The success of a Satellite Launch mission takes into account many factors into consideration with a long planning and a designing procedure. Each phase of the launch vehicle in-flight from launch to reaching the target destination in space is precisely designed and executed. During this process of actually designing a satellite launch the effect of vibrations and its inherent failure and damage mechanics are closely looked upon. When analyzing the vibrations affecting the launch vehicle and the satellite in the pay-load, we closely look at what type of external forces affect the satellite varying from Acoustic pressures, structure-borne vibrations to Aerodynamic excitation.