The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 28, 2016

Filed:

Mar. 15, 2013
Applicant:

Ihi Aerospace Co., Ltd., Tokyo, JP;

Inventors:

Toru Nagao, Tokyo, JP;

Naoki Morita, Tokyo, JP;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 9/00 (2006.01); F02K 9/34 (2006.01); F02K 9/52 (2006.01); F02K 9/60 (2006.01); F02K 9/62 (2006.01); F02K 9/68 (2006.01); F02K 9/97 (2006.01); B64G 1/22 (2006.01); B64G 1/24 (2006.01); B64G 1/26 (2006.01); B64G 1/40 (2006.01); F02K 9/94 (2006.01);
U.S. Cl.
CPC ...
F02K 9/00 (2013.01); B64G 1/22 (2013.01); B64G 1/24 (2013.01); B64G 1/26 (2013.01); B64G 1/40 (2013.01); B64G 1/401 (2013.01); B64G 1/405 (2013.01); B64G 1/406 (2013.01); F02K 9/34 (2013.01); F02K 9/343 (2013.01); F02K 9/52 (2013.01); F02K 9/60 (2013.01); F02K 9/605 (2013.01); F02K 9/62 (2013.01); F02K 9/68 (2013.01); F02K 9/94 (2013.01); F02K 9/97 (2013.01); F05C 2201/0466 (2013.01); F05D 2300/133 (2013.01);
Abstract

A thruster designed to produce thrust by introducing a propellant to a catalyst layer from a propellant valve via a propellant introduction member and spurting out a gas resulting from decomposition of the propellant occurring on the catalyst layer, wherein the thruster comprises a chamber of an Ni alloy for holding the catalyst layer inside, the propellant introduction member is made of an Ni alloy and connects the propellant valve and the chamber, and a propellant valve flange of a Ti alloy with a plurality of columns of a Ti alloy is arranged between the chamber and the propellant valve to support the chamber by the columns.


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