Abstract
Most modern spacecraft are made of three-layer honeycomb panels which are layered structures consisting of two carrier layers and a honeycomb core. When equipment, cables, waveguide networks are installed, a panel has inserts as well. For a spacecraft design to use inserts, it should account for various factors that can affect the bearing capacity of an insert. The study investigates the influence of these factors, tests the method of analytical calculation, and carries out the calculation of inserts. The practical importance of the experimental data obtained makes it possible to use them in honeycomb structures design and calculations.
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