Title:
ホールスラスタ
Document Type and Number:
Japanese Patent JP2014519573
Kind Code:
A
Abstract:
A Hall effect thruster includes at least one tank of gas under high pressure, a pressure regulator module, a gas flow rate control device, an ionization channel, a cathode placed in a vicinity of an outlet from the ionization channel, an anode associated with the ionization channel, an electrical power supply unit, an electric filter, coils for creating a magnetic field around the ionization channel, and an additional electrical power supply unit for applying a pulsating voltage between the anode and the cathode.
Inventors:
The Jur back, Stephen Joseph
The Marchand ディーズ, Frederic
オーベルグ, Michael
The Marchand ディーズ, Frederic
オーベルグ, Michael
Application Number:
JP2014513230A
Publication Date:
August 14, 2014
Filing Date:
May 23, 2012
Export Citation:
Assignee:
It is peevish and a bear.
International Classes:
F03H1/00; H05H1/54
Domestic Patent References:
| JP2006136057A | 2006-05-25 | |||
| JPH11236871A | 1999-08-31 |
Foreign References:
| US20020116915A1 | 2002-08-29 |
Other References:
JPN7016000793; Ｏｌｉｖｉｅｒ Ｄｕｃｈｅｍｉｎ，外４名: '"Ｍｕｌｔｉ-Ｃｈａｎｎｅｌ Ｈａｌｌ-Ｅｆｆｅｃｔ Ｔｈｒｕｓｔｅｒｓ： Ｍｉｓｓｉｏｎ Ａｐｐｌｉｃａｔｉｏｎｓ ａｎｄ Ａｒｃｈｉｔｅｃｔｕｒｅ Ｔｒａｄｅ-Ｏｆｆｓ"' ＩＥＰＣ-２００７-２２７ , 200709, ｐ．１-１５, Ｎａｔｉｏｎａｌ Ｓｐａｃｅ Ｇｒａｎｔ Ｆｏｕｎｄａｔｉｏｎ
JPN6016011834; 大川泰志，外１名: '"パルス型プラズマスラスタの二段放電動作"' 日本航空宇宙学会論文集 第５１巻， 第５９０号, 200303, ｐ．１１４-１１８
JPN6016011834; 大川泰志，外１名: '"パルス型プラズマスラスタの二段放電動作"' 日本航空宇宙学会論文集 第５１巻， 第５９０号, 200303, ｐ．１１４-１１８
Attorney, Agent or Firm:
Yasushi Toyosu
Yasuhiro Toyosu
Hiroyuki Kitani
Yasuhiro Toyosu
Hiroyuki Kitani