DocumentCode :
304172
Title :
Electric rocket thrusters for new spacecraft types with high specific power level
Author :
Grigorian, Vladimir ; Evdokimov, Konstantin ; Izmailov, Azad ; Khartov, Sergey ; Latyshev, Leonid ; Shturlin, Aleksandr
Author_Institution :
Moscow State Aviation Inst., Russia
Volume :
1
fYear :
1996
fDate :
11-16 Aug 1996
Firstpage :
447
Abstract :
The need for small satellites that may be used in space for a long time has grown. One of the driving forces for small satellites to come is the advent of light-weight and long-life solar arrays which are necessary for electric propulsion having long service life. Such a combination of new solar arrays and economical electric thrusters allows relatively cheap, fast and reliable performance of many space missions which can´t be performed using other technologies. This paper describes the development at MAI electric thrusters of 3 types: ion thruster, closed electron drift thruster and a colloidal one. Performance of all these thrusters matches the best world performance for small electrostatic thrusters. These days some of these thrusters are being tested at other organizations
Keywords :
aerospace propulsion; artificial satellites; electron beam applications; ion engines; rocket engines; rockets; MAI electric thrusters; closed electron drift thruster; colloidal thruster; electric propulsion; electric rocket thrusters; high specific power level; ion thruster; small electrostatic thrusters; small satellites; solar arrays; spacecraft; Electrons; Electrostatics; Optical arrays; Propulsion; Rockets; Satellites; Space missions; Space technology; Space vehicles; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Conversion Engineering Conference, 1996. IECEC 96., Proceedings of the 31st Intersociety
Conference_Location :
Washington, DC
ISSN :
1089-3547
Print_ISBN :
0-7803-3547-3
Type :
conf
DOI :
10.1109/IECEC.1996.552924
Filename :
552924
Link To Document :
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