FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering. Proposed transducer consists of two semispherical multilayer PVDF detectors, each comprising thin flexible plates from polarised material with flexible electrodes, calibrated aerogel plate arranged between aforesaid plates, outer heat-insulation damping shield, inner aerogel substrate in contact with said thin flexible plate by one side and, by another side, with transducer semispherical cover. Transducer case is made from nanocomposite material. Said semispherical covers accommodate L-like flanges with seats of flat brackets with clips. Hollow adapter is secured in lower semispherical cover for connection or wires from detector electrodes to electronic unit and transducer mounting at spaceship.
EFFECT: higher reliability and efficiency.
3 cl, 3 dwg
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