Abstract
The method of calculation of efforts on the fasteners of the junction of missile compartments, which have structural features (uneven wall thickness in a circular or longitudinal direction, the presence of openings) under the action of axial forces and bending moments. The technique takes into account the conditions of rocket fastening in the container or vehicle and allows to determine the basic cases and maximum loads on the fasteners for further calculation of the joints for strength. Cite as: V. M. Kharchenko, D. V. Klymenko, “Loading of rocket joins with account for features of constructions of adjacent compartments,” Prykl. Probl. Mekh. Mat. , Issue 17, 98–104 (2019) (in Ukrainian), https://doi.org/10.15407/apmm2019.17.98-104
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