FIELD: radio communication.
SUBSTANCE: invention relates to aircraft radio communication systems. Integrated communication system comprises a shielding housing divided by two additional shielding partitions into three sections, wherein shielding case panels are protective shield to accommodate power buses and high-speed data communication buses. In the first section of the shielding housing there are at least three digital signal processing modules, in the second section there are at least one calculation and switching module, and at least one crypto-imitation protection module, at least three power amplifier modules are placed in the third section, wherein all system modules are high-performance unified printed circuit boards.
EFFECT: reduction of weight and size characteristics due to integrated design of functional modules in a single housing and rejection of cable interunit connectors, improvement of operational reliability and reliability of communication, improvement of operational characteristics of the system at the location object.
1 cl, 2 dwg
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