Abstract
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.
Similar content being viewed by others
REFERENCES
Antropov, N.N., Bogatyi, A.V., D’yakonov, G.A., et al., Development of ablative pulsed plasma thrusters in the Scientific Research Institute of Applied Mechanics and Electrodynamics, Kosmonavt. Raketostr., 2008, no. 3, pp. 28–34.
Antropov, N.N., Bogatyi, A.V., D’yakonov, G.A., et al., New stage of the development of ablative pulsed plasma thrusters in the Scientific Research Institute of Applied Mechanics and Electrodynamics, Vestn. NPO im. S. A. Lavochkina, 2011, no. 5, pp. 30–40.
Bobrov, Yu.K., D’yakov, A.F., Sorokin, A.V., and Yurgelenas, Yu.V., Fizicheskie osnovy elektricheskogo proboya gazov (Physical Bases of Electric Gas Breakdown), Moscow: MEI, 1999.
Gorshkov, O.A., Muravlev, V.A., and Shagaida, A.A., Khollovskie i ionnye plazmennye dvigateli dlya kosmicheskikh apparatov (Hall and Ion Plasma Thrusters for Space Vehicles), Moscow: Mashinostroenie, 2008.
Bogatyi, A.V., D’yakonov, G.A., Nechaev, I.L., et al., Prospects of improving dimensional characteristics of ablative pulsed plasma thrusters, Tr. VNIIEM: Vopr. Elektromekh., 2013, vol. 133, no. 2, pp. 19–26.
Antipov, A.A. and Bogatyi, A.V., Simulation of the motion of charged particles in an ablative pulsed plasma thruster at the initial stage of discharge, Izv. Ross. Akad. Nauk: Energ., 2017, no. 3, pp. 42–49.
Antipov, A.A., Bogatyy, A.V., and Semenov, A.A., Investigation of the initial stage of the discharge in an ablative pulsed plasma thruster, J. Surf. Invest.: X-ray, Synchrotron Neutron Tech., 2018, vol. 12, no. 5, pp. 1037–1040.
Vazhov, V.F. and Lavrinovich, V.A., Tekhnika vysokikh napryazhenii (Technology of High Voltages), Tomsk: TPU, 2008.
Author information
Authors and Affiliations
Corresponding author
Additional information
Translated by V. Arutyunyan
Rights and permissions
About this article
Cite this article
Bogatyi, A.V., D’yakonov, G.A. & Semenikhin, S.A. Mechanisms for the Formation of Parasitic Propellant Consumption in an Ablative Pulsed Plasma Thruster. Cosmic Res 57, 310–316 (2019). https://doi.org/10.1134/S0010952519050010
Received:
Revised:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1134/S0010952519050010