Simulating discharge in communication satellites
The enormous cost of developing and placing a satellite in orbit must be recovered during its useful life
Communication satellites are complex instruments, whose systems and components must pass strict laboratory controls and tests. The enormous cost of developing and placing a satellite in orbit must be recovered during its useful life, providing the greatest possible range of services (television, telephony, Internet, etc.) with the greatest possible number of independent channels.
The growing demand for services means that components must be miniaturised and the number of operative frequencies increased. To service larger areas of the earth's surface and a greater number of users, the strength of the radio frequency transmitted must be high, creating ideal conditions for the formation of unwanted destructive discharges: intense microwave electric fields inside small spaces within the satellite's communication system. Similar circumstances can be found in other complex systems using microwaves, such as particle accelerators or semiconductor materials processing equipment.
Microwave systems used in communication satellites must operate under extreme conditions with high-strength radio frequency. Their communication performance must be optimal and the possible appearance of destructive discharges must be predicted. A group of researchers at the Autonomous University of Madrid (UAM) is currently working on numerical simulations that predict the formation of destructive discharges. Numerical simulations save the costs of testing laboratory equipment and give designers extremely useful information on the limits and operating conditions of the equipment.
Electric discharges consist of multiple charges. The two basic processes caused by microwaves are called multipactor and corona discharges. The first occurs at very low gas pressures (typically below 10-5 mBar), when electrons, accelerated by the electric field of the microwave, impact a surface (metallic or dielectric), causing emission of a new secondary electron. Multipactor discharge is caused by this repeated multiplication of secondary electrons, with the properties of the materials playing a crucial role. Corona discharge occurs at very high pressures (above 10-2 mBar) because of ionisation of the residual gas filling the device, with the properties of the materials also playing a crucial role. Between both pressure bands, there is a transition zone where both charge multiplication mechanisms exist, called multipactor collisional.
Three members of the GHIA group from the Department of Computer Engineering of the UAM, in collaboration with Professor Luis Conde of the Universidad Polit¨¦cnica de Madrid (UPM) and David Raboso of the European Space Agency, have recently published a paper in PHYSICAL REVIEW E reporting on multipactor and corona discharge prediction in wave guides through simulation. Specifically, their system can be used in the transition pressure range, where until now simulation tools have been unavailable, and the results obtained for low and intermediate pressures have been validated with experimental data published in the scientific literature.
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