ELECTRIC PROPULSION IN RUSSIA AND ITS PRACTICAL APPLICATIONS

Citation
Ga. Popov et Ya. Ryzhov, ELECTRIC PROPULSION IN RUSSIA AND ITS PRACTICAL APPLICATIONS, Zeitschrift fur Flugwissenschaften und Weltraumforschung, 17(3), 1993, pp. 161-169
Citations number
NO
Categorie Soggetti
Aerospace Engineering & Tecnology
ISSN journal
0342068X
Volume
17
Issue
3
Year of publication
1993
Pages
161 - 169
Database
ISI
SICI code
0342-068X(1993)17:3<161:EPIRAI>2.0.ZU;2-M
Abstract
Since the end of the 50's, practically all known EP-thruster types hav e been investigated in the USSR. Since the first flight tests in 1964, more than 50 EP-thrusters were flown for satellite-orbit correction a nd more than 30 EP-engines were used for active ion & plasma experimen ts in space as well as for spacecraft discharging. Presently, the Russ ian EP-program is focussed on the stationary plasma thruster type with closed drill of electrons, suggested by A.I. Morosov and industrializ ed by 'Fakel Enterprise', Kaliningrad. Different-sized engines of this 'SPT'-type have been developed, qualified and flown. Besides this typ e, also pulsed plasma thrusters with ablating solid propellant 'PPT', MPD-engines with applied and self-magnetic field as well as bombardmen t ion engines have been under R, D & Q-work and were flown. The Moscow Aviation Institute gave important contributions for all this work. In Russia, plasma and ion thrusters are also used for non-propulsive, te chnological applications, e.g. for material processing.