Author:
Perov S N,Glushkov S V,Stepanets D V
Abstract
Abstract
A typical three-layer honeycomb panel of a spacecraft (SC) is considered. For connection to the power frame of the spacecraft, as well as for rigging works, embedded elements (inserts) are installed in the panel. The results of experimental and numerical determination of the bearing capacity of the panel in the places of installation of potted inserts under the action of the load in its plane are presented in the article.
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