FIELD: aircraft and rocket equipment.
SUBSTANCE: invention relates to aircraft and rocket equipment, particularly to antenna fairings of high-speed rockets of various classes. In antenna fairing containing ceramic shell, butt metal butt and a dome-shaped radiotransparent heat shield coaxially attached by means of a heat-resistant adhesive to the shell and a frame through the heat-insulating ring, said heat shield is made of two or more layers with sealed inner layer of fiberglass, and in the frame there is a system of holes for releasing excess pressure.
EFFECT: technical result is to ensure tightness of the inner volume of the radiotransparent fairing, in which the structure equipment is located, under conditions of high-temperature heating with simultaneous protection of the equipment against overheating.
3 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
ANTENNA FAIRING | 2020 |
|
RU2738428C1 |
ANTENNA DOME | 2013 |
|
RU2536360C1 |
ANTENNA DOME | 2017 |
|
RU2659586C1 |
ANTENNA FAIRING | 2018 |
|
RU2679483C1 |
ANTENNA DOME | 2017 |
|
RU2644621C1 |
ANTENNA DOME | 2013 |
|
RU2536339C1 |
ANTENNA FAIRING | 2018 |
|
RU2694132C1 |
ANTENNA FAIRING | 2020 |
|
RU2738429C1 |
ANTENNA FAIRING | 2020 |
|
RU2735359C1 |
ANTENNA DOME | 2019 |
|
RU2748531C1 |
Authors
Dates
2020-12-14—Published
2020-04-24—Filed