Dual-polarization waveguide feed chains are a key sub-system in most radio frequency (RF) satellite payloads as well as reflector based ground antennas. For example, horn antennas are commonly used as part of reflector and array antenna sub-systems in RF satellite payloads because of their high performance and low insertion losses. They are generally fed by orthomode transducers (OMT) or orthomode junctions (OMJ), enabling polarization diversity and/or multiple frequency operation, typically at least transmit (Tx) and receive (Rx) bands.
Four-probe OMT designs were for a long time the preferred approach, as this symmetric design naturally provides high-order modes rejection. A typical approach to achieve high performance is to have the 4-probe OMT closer to the horn operating in the lower frequency band (Tx band for the onboard feed chains). A typical 4-probe design will have a footprint diameter of about 5/6 wavelengths at the highest operating frequency (e.g. 50 to 60 mm at 30 GHz), including the probe filters and combining network (for linear or circular polarization operation).
However, with the advent of high throughput satellites (HTS), requiring hundreds of beams and hence, hundreds of feed chains, the reduction of the footprint of feed chains without compromising performance has become a prime issue.
As mentioned above, the pior art found is characterized by a common waveguide having a cross section with a discrete rotational symmetry of order 4 (e.g. circular, square). This is to provide similar operation for the two orthogonal components of the coupled electric field.