DocumentCode
3115454
Title
Development of small scale microwave discharge ion thruster of 3–5 cm size
Author
Takao, Y. ; Iwata, I. ; Nan Chyou
Author_Institution
Dept. of Digital Eng., Nishinippon Inst. of Technol., Japan
fYear
2012
fDate
9-12 Oct. 2012
Firstpage
497
Lastpage
499
Abstract
Development of microwave discharge ion thrusters of 3cm size thruster was conducted to confirm the design approach to small scale microwave discharge ion thrusters, and concept of 5cm size thruster improved in plasma ignition and sustention was reported. As we have already developed 10cm and 2cm size microwave discharge type ion thrusters, the development of 3cm one on the basis of the previous ones is carried out. It is sometimes difficult to generate plasma in the 5cm size microwave discharge ion thruster. Several magnetic configurations in the discharge chamber were calculated for the development of 5cm thruster with variable magnetic field.
Keywords
high-frequency discharges; ignition; ion engines; plasma production; discharge chamber; magnetic configurations; magnetic field; plasma generation; size 10 cm; size 3 cm to 5 cm; small scale microwave discharge ion thruster; Magnetostatics; NASA;
fLanguage
English
Publisher
ieee
Conference_Titel
Vehicle Power and Propulsion Conference (VPPC), 2012 IEEE
Conference_Location
Seoul
Print_ISBN
978-1-4673-0953-0
Type
conf
DOI
10.1109/VPPC.2012.6422749
Filename
6422749
Link To Document