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- W4320160480 abstract "The small closed volume occupied by cold gas plasma is a feature of the orbit-correction propulsion systems of spacecraft (PSSC). When determining the kinetic parameters of the working fluid flow in the arcjet and argon is selected as the process gas, the most important characteristic is the gas temperature. The well-known statement about the adiabatic nature of the compression process due to an increase in temperature suggests that the compression process is a source of natural gas oscillations and is of paramount importance for establishing the Boltzmann distribution of excited atoms over energy levels. In the Boltzmann approximation, using the methods of emission spectroscopy, the temperature of the working gas in the PSSC was obtained which made it possible to determine the effective flow rate of argon and the corresponding speed of sound. The values of the kinetic parameters of the supersonic argon flow in the arcjet made it possible to substantiate the results of recording the frequency of oscillations of the arc voltage of the PSSC discharge chamber in the Helmholtz resonator mode near fH= 6.25 kHz. It is shown that the length of the discharge chamber in the approximation of a partially open resonator can be of decisive importance in finding the natural vibrations of the resonator. It is suggested that on the basis of the engine under consideration, it is possible to consider the initiation of detonation in a supersonic flow of a combustible mixture." @default.
- W4320160480 created "2023-02-13" @default.
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- W4320160480 date "2021-06-30" @default.
- W4320160480 modified "2023-09-29" @default.
- W4320160480 title "SUPERSONIC ARGON FLOW PARAMETERS IN AN ARCJET THRUSTER" @default.
- W4320160480 doi "https://doi.org/10.30826/icpcd12b17" @default.
- W4320160480 hasPublicationYear "2021" @default.
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