A GMSK VHF-uplink/UHF-downlink transceiver for the CubeSat missions

Abstract

Functional and thermal performance characteristics of a Very High Frequency/Ultra High Frequency (VHF/UHF) transceiver based on Gaussian Minimum Shift Keying (GMSK) modulation are presented. The transceiver has been designed for CubeSats telemetry and commanding needs or low rate data download. The design is validated at 27 dBm, 30 dBm and 33 dBm transmitting powers over −20 • C to +51 • C. Under these thermal conditions, the transmitter spurious dynamic response shows little if any change and the average sensitivity of receiver at the 12 dB SIgnal Noise And Distortion (SINAD) is −116.7 dBm at 140 MHz and −116.78 dBm at 149.98 MHz. The transmitter and receiver frequencies are stable and the current consumption as well the output RF levels are steady. The design has been verified against a simulation model which allows system tradeoff analysis. The measurements demonstrate the transceiver made with commercial grade parts has dependable performance at the low earth altitudes and orbital heating conditions.

Space Environment Evaluation and Low-Earth-Orbit Demonstration of a Communication Component with a Commercial Transceiver Integrated Circuit

“…At present, only one company produces communication devices for space applications that combine consumer integrated circuits (ICs) with discrete components for the 144 and 430 MHz amateur frequency bands used by many universities [8]. This communication equipment is highly reliable and has been used by several universities in Japan; however, currently, Japanese research on communication equipment and antennas is lagging behind the experimental and pioneering work being conducted in other countries [9,10]. Although detailed experimental research on Doppler shift tolerance in the 434 MHz band using the CubeSat LoRa module has been reported [11], few studies have evaluated the radiation tolerance of consumer electronic components for potential use in CubeSat; such evaluations are important to determine component feasibility for space application.…”