FIELD: aircraft and rocket equipment.
SUBSTANCE: invention relates to the field of aircraft and rocket equipment and can be mainly used in production of aerial fairings of "air-surface" or "air-air" rockets. Antenna fairing with combined radio and optical channels includes a thin-walled shell from composite radiotransparent material with an optical window located in the nose part of the shell. Optical opening has shape of outer surface, which is continuation of outer contour of shell, and is connected to it by elastic glue-sealant, shell wall in connection with window has a form of Z-shape, and the optical thicknesses of the optical window and shell have different values and are selected in accordance with the number of half-wave lengths in the radio range.
EFFECT: technical result consists in provision of efficiency of fairing in radio and optical range, optimization of loads on optical element and increase in strength of connection of optical window with shell.
1 cl, 2 dwg
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Authors
Dates
2019-10-11—Published
2019-02-04—Filed