Forecasting longitudinal vibrations of spacecraft structure and equipment during the operation of pyrotechnics

Abstract

 The article analyzes the effect of an energy impulse from pyrotechnics, presents models and methods for calculating vibration overload, which make it possible to predict the vibration load of the spacecraft compartment and spacecraft equipment, taking into account the shock absorber. The efficiency of the presented approaches is illustrated with specific examples. The obtained results can be useful to engineering and technical specialists of organizations, as well as to students of the corresponding educational field.