Development and testing pre-models of high damping rod element based on graphite-epoxy with actuator functions
The discussed problems with the development of prototypes of elements of high-damping, suitable for the effective damping in the designs of spacecraft. The results of numerical analysis of high-damping elements that based on carbon plastics with executive functions carried out by using specially designed software. These results are compared with experimental data obtained in the tests established in damping system based on piezoelectric actuators and gyrator.