DISCHARGE PLASMA REACTION TYPE THRUSTER - JAPAN AEROSPACE EXPLORATION

Title:

DISCHARGE PLASMA REACTION TYPE THRUSTER

Document Type and Number:

Japanese Patent JP2006037824

Kind Code:

A

Abstract:

To provide a thruster not using a catalyst for attitude control of a rocket and an artificial satellite.

The thruster decomposing and burning material including high molecular compound by using discharge plasma of the material without substantial intervention of a catalyst and promoting combustion is provided.

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Inventors:

NAGASHIMA RYUICHI
SAITO KENKICHI
TAKEGAHARA HARUTAKA
AOYANAGI JUNICHIRO
KURIKI KYOICHI
TACHIBANA TAKESHI
KAGAMI SATOSHI
NAKAJIMA SHOJI
MISHIMA HIROYUKI

Application Number:

JP2004218130A

Publication Date:

February 09, 2006

Filing Date:

July 27, 2004

Export Citation:

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Assignee:

JAPAN AEROSPACE EXPLORATION
MITSUBISHI HEAVY IND LTD

International Classes:

F03H1/00

Attorney, Agent or Firm:

Sadao Kumakura
Fumiaki Otsuka
Toshio Imajo
Takaki Nishijima

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