FIELD: space technology.
SUBSTANCE: invention relates to the field of space technology, specifically to assembly method for a unified spacecraft platform (USCP) body. The assembly method for USCP is carried out with the vertical position of the racks. Lower parts of the primary structure (PS) are connected to the first supporting transverse honeycomb panel lying in the XOZ plane through end fittings. Intermediate transverse honeycomb panels are mounted between flanges of the end fittings. Connect ends of the racks with the second supporting transverse honeycomb panel. Mechanical processing of embedded elements installed in racks is carried out to obtain the necessary interface surfaces, on which separate longitudinal honeycomb panels are installed alternately. Install longitudinal honeycomb panels parallel to the XOY plane, and then parallel to the ZOY plane. Each of the installed longitudinal honeycomb panels is independently connected to the PS.
EFFECT: installation safety is achieved.
1 cl, 7 dwg
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Authors
Dates
2021-12-14—Published
2021-05-05—Filed