FIELD: rocket equipment.
SUBSTANCE: invention relates to the aircraft and rocket equipment and can be used for the antenna fairings production of high-speed missiles of various classes with shells of heat-resistant ceramic materials. Antenna cowl includes a ceramic shell connected by a heat-resistant adhesive to a metal frame consisting of an adapter with through slots uniformly arranged in circumferential direction, and a butt element interconnected by means of collars, pins and a sealing ring. In the nose part of the adapter between the through grooves there are in-through slots forming lobes with length of 0.5–0.7 of the adapter height, wherein the through slots overlap the through slots in the nose part of adapter by 0.2–0.3 of the height of the adapter, and the lobes are made with rounding.
EFFECT: increased strength reliability of the antenna cowling, simplified design and increased reliability of gluing.
1 cl, 3 dwg
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Authors
Dates
2019-05-30—Published
2018-09-20—Filed