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In this paper we describe the development of a compact and lightweight reconfigurable 4×4 switch matrix module for geostationary satellite communications in Ka-band (17…22 GHz), where signal routing becomes more and more relevant. The module is based on a space-qualified low-temperature co-fired ceramic multilayer technology. Following a successful on-orbit verification aboard a low-earth orbit satellite mission, the switch matrix has undergone major design revisions, aiming at an industry-scale manufacturability without compromising the advanced functional performance. By applying a system-in-package approach including automated hybrid assembly, a fully operational breadboard version has been developed, which upon further space qualification steps is intended to become part of a reconfigurable input multiplexer aboard the geostationary Heinrich Hertz satellite. Combining a ceramic package, an organic multilayer interface, wire-bonded coaxial connectors into an aluminum housing, the dimensions measure 126 mm × 87 mm × 11 mm with a weight of 193 g, corresponding to a reduction of 60 % in volume and 40 % in mass compared to a previous electronic version, and orders-of-magnitude better than coaxial switch matrices.

The ongoing developments of satellite antenna technology, mainly of multiple-feed-per-beam (MFB) concepts, combined with advanced compound semiconductor and packaging technologies that provide the building blocks for a new generation of K-band satellites, are reported. This paper proposes a next-generation MFB application scenario using the advantages of both new antenna and solid-state power amplifier concepts.