FIELD: rocket equipment.
SUBSTANCE: invention relates to the field of aircraft and rocket equipment and can be mainly used in production of ceramic antenna fairings of high-speed surface-to-air missiles. Fairing comprises a ceramic shell, a metal adapter connected by means of an elastic adhesive to the inner surface of the shell. Adapter end is rigidly attached to or made integral with the shell shifted towards nose by a value not less than the thickness of the shell at its end, a stiffness compensator in the form of a ring shell protruding beyond the end of the shell, and wall thickness of not less than 1/3 of wall thickness of adapter at its end face, wherein protruding part of shell is made with fastening collar in the form of sectors uniformly located along its perimeter, which outer diameter is commensurable with outer diameter of adapter at its end, besides, stiffness compensator dimensions are specified by calculation with allowance for plasticity in its most loaded area.
EFFECT: increase of temperature and power operational parameters of ceramic fairings of rockets and increase of their carrying capacity.
1 cl, 1 dwg
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Authors
Dates
2019-05-30—Published
2018-08-27—Filed