Investigation of erosion and deposition in a microwave discharge neutralizer

Naoji Yamamoto, Yushi Maeda, Hideki Nakashima, Hiroki Watanabe, Ikkoh Funaki

Research output: Contribution to journalArticle

2 Citations (Scopus)

Abstract

A one hundred hour test of a 100mA class microwave discharge neutralizer was performed to investigate the erosion rate and deposition in the neutralizer. The mass loss of each component (antenna, discharge chamber wall, front yoke, back yoke, insulator and orifice) was measured in diode mode (contact voltage of 50 V) at a constant incident microwave power of 8W and xenon mass flow rate of 49 μg/s. The measured erosion rates of the discharge chamber and the antenna were 180 μg/hr and 10 μg/hr, respectively. The element concentration of the deposited material on the back yoke and insulator were measured; the contamination on the insulator was found to contain 34% copper from the wall and 6% molybdenum from the antenna.

Original languageEnglish
Pages (from-to)100-103
Number of pages4
JournalTransactions of the Japan Society for Aeronautical and Space Sciences
Volume59
Issue number2
DOIs
Publication statusPublished - Jan 1 2016

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neutralizers
erosion
antenna
Erosion
Microwaves
insulators
Antennas
erosion rate
microwaves
antenna components
antennas
chambers
xenon
mass flow rate
Xenon
orifices
Orifices
molybdenum
Molybdenum
Diodes

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

Cite this

Investigation of erosion and deposition in a microwave discharge neutralizer. / Yamamoto, Naoji; Maeda, Yushi; Nakashima, Hideki; Watanabe, Hiroki; Funaki, Ikkoh.

In: Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 59, No. 2, 01.01.2016, p. 100-103.

Research output: Contribution to journalArticle

Yamamoto, Naoji ; Maeda, Yushi ; Nakashima, Hideki ; Watanabe, Hiroki ; Funaki, Ikkoh. / Investigation of erosion and deposition in a microwave discharge neutralizer. In: Transactions of the Japan Society for Aeronautical and Space Sciences. 2016 ; Vol. 59, No. 2. pp. 100-103.
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