Abstract.A one-dimensional compressible fluid calculation was coupled with a finitedifference time-domain code and a particle-in-cell code with collision to reproduce propagation of electromagnetic wave, ionization process of plasma, and shock wave formation in atmospheric microwave discharge. Plasma filaments are driven toward the microwave source at 1 atm, and the distance between each filament is one-fifth of the wavelength of the incident microwave. The strong shock wave is generated due to the high plasma density at the atmospheric pressure. A simple analysis of the microwave propagation into the plasma shows that cut-off density of the microwave becomes smaller with the pressure decrease in a collisional plasma. At the lower pressure, the smaller density plasma is obtained with a diffusive pattern because of the smaller cut-off density and the larger diffusion effect. In contrast with the 1-atm case, the weak shock wave is generated at a rarefied condition, which lowers performance of microwave thruster.
IntroductionSignificant advancement for space transportation is needed to utilize an outer space as academic study, space travel, military defense, weather observation and so on. Recently, microwave propulsion system has been investigated to launch a small satellite with saving operation cost by high-power energy transmission from a microwave oscillator established on a ground. The irradiated microwave is focused by a parabolic mirror installed on the vehicle, and the intense microwave generates a plasma with sustaining a strong shock wave which supplies an impulsive thrust through interactions with the rocket thruster. In past experiments of the plasma formation by the microwave [1][2][3], filamentary arrays of the plasma were observed in contrast with a bulk plasma obtained in a laser breakdown [4]. The plasma filaments propagate toward the microwave source at km/s-order velocity, and the distance between each filament is about one-quarter of the incident microwave wavelength. However, at the lower pressure, the plasma cannot form the filamentary structure, and the measured impulse of the microwave rocket drastically drops down [2,3]. Detailed mechanism of the thrust decrease is not identified by the past experiments; therefore, the plasma and shock generations by the microwave discharge should be examined.In this study, we have developed a one-dimensional integrated simulator by combining a finitedifference time-domain (FDTD) code, a particle-in-cell with Monte Calro collision (PIC-MCC) code, and a computational fluid dynamics (CFD) code to assess the shock wave and plasma formations by the microwave discharge. We then numerically assess the ambient pressure effects for the plasma and shock wave structures, and specify the mechanism of the thrust decrease at the lower pressure.