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:
Apr. 06, 2021

Filed:

May. 17, 2017
Applicant:

Airbus Ds Gmbh, Taufkirchen, DE;

Inventors:

Ulrich Gotzig, Bad Friedrichshall, DE;

Malte Wurdak, Moeckmuehl, DE;

Joel Deck, Neudenau, DE;

Manuel Frey, Munich, DE;

Assignee:

ARIANEGROUP GMBH, Taufkirchen, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 9/68 (2006.01); F02K 9/64 (2006.01); F02K 9/95 (2006.01); F02K 9/42 (2006.01); F02K 9/44 (2006.01);
U.S. Cl.
CPC ...
F02K 9/64 (2013.01); F02K 9/425 (2013.01); F02K 9/44 (2013.01); F02K 9/68 (2013.01); F02K 9/95 (2013.01); F05D 2220/80 (2013.01); F05D 2240/35 (2013.01); F05D 2260/202 (2013.01); F05D 2260/2212 (2013.01);
Abstract

A rocket propulsion system comprises a combustion chamber, an oxygen supply system, comprising an oxygen supply duct and being configured to supply oxygen to the combustion chamber, and a hydrogen supply system, comprising a hydrogen supply duct and being configured to supply hydrogen to the combustion chamber. An ignition unit of the propulsion system, to which at least portions of the oxygen and the hydrogen supplied to the combustion chamber can be supplied, is configured to initiate combustion of the oxygen-hydrogen mixture in the combustion chamber. The propulsion system further comprises a cooling duct extending along an inner surface of a combustion chamber wall and through which at least a portion of the oxygen supplied to the combustion chamber, at least a portion of the hydrogen supplied to the combustion chamber or a combustion gas mixture emerging from the ignition unit flows.


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