Currently, all existing waveguide feed systems in SATCOM reflector antennas are the aggregation of various well-known components designed as stand-alone elements. This restricts the minimum achievable volume. The current state-of-the-art in Europe for broadband dual-band dual-polarisation K/Ka feed systems of interest for SATCOM payloads, including very high throughput satellite (VHTS) multiple beam antenna systems impose a feed spacing of 30 mm or larger, which may result in (too) large satellite antennas or significant performance degradation due to e.g., high grating lobes within the field of view. Future payloads, including ultra-high throughput satellite (UHTS) with higher spectral density, would benefit from smaller feeds, and in particular feeds with a reduced footprint in the focal plane, without compromising its length.
The very compact design introduced with this invention is based on a co-design of the different feed components. This leads to the design of a developable H-plane coupler referred to as rooftop coupler, which is the key innovation, as well as an assembly of this component with the previously developed compact two-probe OMT (ESA PAT 747) and an in-line filter design. The solution developed fits in a lattice of only 20 mm, which corresponds to a reduction in volume by a factor of two compared to prior art when implemented using screwless assembly techniques.
In this H-plane coupler, the H-plane is mapped to a developable surface such as a cylinder or a parallelepiped. Two examples of developable couplers are reported in Fig. 1.