FIELD: aviation.
SUBSTANCE: sensor for researching meteoroid flows and man-made particles in space is designed in the form of a cube, all faces of which are composite detectors, consisting of internal and external sensing elements, the external sensing elements are made of a thin film with a number of cells with conductive track and the internal sensing elements - of a volume polarized PVDF film. The sensor housing is designed in a form of a frame of a nanocomposite material, a fastening is set on one of the planes to connect with the spacecraft by means of external rod with extending flexible information loops through it. Frames with composite detectors are set on the frame.
EFFECT: possibility of complex spatial registration of meteoroid and man-made particles, determination of their parameters.
5 dwg
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Authors
Dates
2017-05-11—Published
2016-03-09—Filed