FIELD: information technology.
SUBSTANCE: invention relates to radio equipment and can be used in space and/or aviation technology for transmitting/receiving information via a high-speed radio link in the space-to-space and/or space-to-aerial vehicle directions. To realise the described result, information is transmitted/received with a coordinated right and/or left circular polarisation of radio waves between the transmitting/receiving antennas using a high-speed radio link at hyperhigh frequencies (HHF) in the range from 300 to 1000 GHz of the electromagnetic spectrum between space vehicles (SVs) located on low, medium, highly elliptical and geostationary orbits, and/or unmanned aerial vehicles (UAVs) at altitudes of 7 km and above. The transmitting hyperhigh-frequency antennas are located on the SVs and/or the UAVs, wherein one horn or parabolic antenna is placed on each vehicle, transmitting with both right and left circular polarisation, and the receiving hyperhigh-frequency antennas are located on board of the space vehicles and/or unmanned aerial vehicles, wherein an antenna system consisting of N horns is placed on each vehicle.
EFFECT: provided is continuous two-way transmission of data between SVs located in low, medium, highly elliptical and geostationary orbits.
1 cl, 1 dwg
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