“…For a given mission scenario, the specific advantages and disadvantages of the MBA solutions with the associated frontends have to be carefully traded-off in terms of performances (e.g., directivity, C/I, system capacity), power requirements, hardware complexity, reliability, redundancy, reconfigurability, accommodation (i.e., mass, envelope, number and size of reflectors), and costs. The comparison among different MBAs for some relevant mission scenarios are reported in [9], [14], [15]. As an example, Viasat-3, a global system comprising three GEO satellites and expected to be launched early 2023, is anticipated to deliver at least 1 Tbps per satellite, each with a coverage having more than 2000 beams (Fig.…”