Ga. Popov et Ya. Ryzhov, ELECTRIC PROPULSION IN RUSSIA AND ITS PRACTICAL APPLICATIONS, Zeitschrift fur Flugwissenschaften und Weltraumforschung, 17(3), 1993, pp. 161-169
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.