The Integrated Structure Design for the Transmitter of the Companion Satellite

Abstract

The integrated structure design for the transmitter, for use in the Companion Satellite (BX-1) in SZ-7 flight mission, is described. Based on the single-layer structure with several grooves formed on both sides, the miniaturization and high reliability is achieved while offering uncompromised electromagnetic compatibility (EMC) and convenience for assembly and disassembly.