TECHNICAL MECHANICS
ISSN (Print): 1561-9184, ISSN (Online): 2616-6380
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UDC 533.27.539.2
Technical mechanics, 2014, 1, 105 - 110
CHARACTERISTIS OF ELECTRICAL JET ENGINE OF HALL-TYPE FOR CORRECTION OF MICROSATELLITES ORBITS
Kulagin S. N.
| ABSTRACT |
The research aim is to define the degree of influence of the discharge voltage on thrust performance
and power characteristics of the ITM-31 Hall low-powered engine developed at the Institute of Technical
Mechanics of the National Academy of Sciences of Ukraine and State Space Agency of Ukraine. Control
characteristics in a power range of 18-304 W are presented. The evaluation of an allowable operating
range of the discharge voltage is pioneered. The practical importance is to increase the efficiency
of the Hall engine for minimizing the power consumption.
| KEYWORDS |
discharge voltage, thrust and power characteristics, electrical jet engine of Hall-type, control characteristics, microsatellites orbits
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| REFERENCES |
1. Gorshkov O. A. Hall and Ion Plasma Engines for Spacecraft (in Russian) / O. A. Gorshkov, V. A. Muravlev, A. A. Shagayda. – Moscow: Mashinostroyenie, 2008. – 280 p.
2. Loyan A. V. Studies of plasma parameters through channel of low-pressure engine at increased charge voltages (in Russian) / A. V. Loyan, T. A. Maksimenko, N. N. Koshelev // Aviatsionno-Kosmicheskaya Tekhnika i Tekhnologia. – 2011. – Vol. 4(81). – P. 53 -57.
Copyright (©) 2014 Kulagin S. N.
Copyright © 2014-2018 Technical mechanics
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