DocumentCode
1622375
Title
Development of Space Propulsion Experiment (SPEX) Device with a Helicon Plasma Source
Author
Uhm, Jang-Won ; Woo, Hyun-Jong ; Chung, Kyu-Sun
Author_Institution
Hanyang Univ., Seoul
fYear
2007
Firstpage
497
Lastpage
497
Abstract
Summary form only given. The helicon plasma source has been developed for the Space Propulsion Experiments (SPEX) with 13.56 MHz RF frequency. This plasma source is attached in the DiPS (Diversified Plasma Simulator). The SPEX is composed of three parts such as helicon source, magnetic compression region and expansion region. The magnetic field geometry is similar to the VASIMR concept but its magnitude is different such as 500 G (at source region), 1.5 kG (at magnetic compression region). Helicon plasma is generated by the m= 1 antenna with the diameter of 4 cm and 12 cm long. The initial plasma parameter has been measured by the optical emission spectroscopy and single Langmuir probe with axial position (compression and expansion region), magnetic field intensity, operating pressure and operating gases (He and Ar).
Keywords
aerospace propulsion; magnetic fields; plasma diagnostics; plasma simulation; plasma sources; diversified plasma simulator; expansion region; frequency 13.56 MHz; helicon plasma source; magnetic compression region; magnetic field geometry; magnetic field intensity; magnetic flux density 1.5 kG; magnetic flux density 500 G; operating gases; operating pressure; optical emission spectroscopy; size 12 cm; size 4 cm; space propulsion experiments; Antenna measurements; Geometry; Magnetic field measurement; Magnetic fields; Plasma devices; Plasma measurements; Plasma simulation; Plasma sources; Propulsion; Radio frequency;
fLanguage
English
Publisher
ieee
Conference_Titel
Plasma Science, 2007. ICOPS 2007. IEEE 34th International Conference on
Conference_Location
Albuquerque, NM
ISSN
0730-9244
Print_ISBN
978-1-4244-0915-0
Type
conf
DOI
10.1109/PPPS.2007.4345803
Filename
4345803
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