Mechanisms for the Formation of Parasitic Propellant Consumption in an Ablative Pulsed Plasma Thruster

Results of spectroscopic studies of electric discharge stages in the channel of an ablative pulsed plasma thruster (APPT) are presented. The initial stage has been shown to affect further discharge development. Shock surface ionization of the propellant has been found to be the dominant mechanism fo...

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Veröffentlicht in:	Cosmic research 2019-09, Vol.57 (5), p.310-316
Hauptverfasser:	Bogatyi, A. V., D’yakonov, G. A., Semenikhin, S. A.
Format:	Artikel
Sprache:	eng
Schlagworte:	Ablation Astronomy Astrophysics and Astroparticles Astrophysics and Cosmology Dependence Electric discharges Ionization Physics Physics and Astronomy Propellant consumption Space Exploration and Astronautics Space Sciences (including Extraterrestrial Physics Surface ionization
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container_title	Cosmic research
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creator	Bogatyi, A. V. D’yakonov, G. A. Semenikhin, S. A.
description	Results of spectroscopic studies of electric discharge stages in the channel of an ablative pulsed plasma thruster (APPT) are presented. The initial stage has been shown to affect further discharge development. Shock surface ionization of the propellant has been found to be the dominant mechanism for “parasitic” propellant consumption of an APPT. The results of experimental studies of the dependence of propulsion efficiency and consumption on the distance between operating surfaces of APPT propellant bars are given.
doi_str_mv	10.1134/S0010952519050010
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subjects	Ablation Astronomy Astrophysics and Astroparticles Astrophysics and Cosmology Dependence Electric discharges Ionization Physics Physics and Astronomy Propellant consumption Space Exploration and Astronautics Space Sciences (including Extraterrestrial Physics Surface ionization
title	Mechanisms for the Formation of Parasitic Propellant Consumption in an Ablative Pulsed Plasma Thruster
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