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:
Jul. 06, 2021

Filed:

May. 18, 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 9/56 (2006.01); F02K 9/64 (2006.01); F02K 9/95 (2006.01); F02K 9/58 (2006.01); F02K 9/42 (2006.01);
U.S. Cl.
CPC ...
F02K 9/56 (2013.01); F02K 9/425 (2013.01); F02K 9/58 (2013.01); F02K 9/64 (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 method for operating a rocket propulsion system comprises the steps of supplying oxygen to a combustion chamber, supplying hydrogen to the combustion chamber and combusting the oxygen-hydrogen mixture in the combustion chamber. The rocket propulsion system is operated alternately in a first operating mode, in which oxygen and hydrogen are supplied to the combustion chamber in a first mass mixing ratio of oxygen to hydrogen, and in a second operating mode, in which oxygen and hydrogen are supplied to the combustion chamber in a second mass mixing ratio of oxygen to hydrogen that is greater than the first mass mixing ratio.


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