I. Introduction
The increasing demand for high-speed, low-latency global connectivity is driving the development of low-Earth-orbit (LEO) and medium-Earth-orbit (MEO) satellite communications (SATCOMs) [1], [2], [3], [4], [5], [6], [7], [8], [9]. To address the significant free-space path loss, phased-array systems are widely used to create steerable directional beams, enhancing the high signal-to-noise ratio (SNR) [10]. Moreover, the equivalent isotropically radiated power (EIRP) improved by the spatial power combining in large transmitter phased arrays relieves the need for output power per element, facilitating the use of cost-effective, high-integration CMOS technologies with limited output power capacity [11]. However, the satellite’s physical size limits the dimensions of the phased arrays, thereby constraining the number of beamformers. Consequently, a coaperture multibeam phased array is proposed to process independent data streams from different directions concurrently with a reduced antenna array size, as illustrated in Fig. 1.
Multibeam application of the SATCOM.