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.
Patent No.:
Date of Patent:
Oct. 12, 2021
Filed:
May. 18, 2017
Applicant:
Airbus Ds Gmbh, Taufkirchen, DE;
Inventors:
Ulrich Gotzig, Bad Friedrichshall, DE;
Malte Wurdak, Moeckmuehl, DE;
Assignee:
Arianegroup GmbH, Taufkirchen, DE;
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 9/64 (2006.01); F02K 9/68 (2006.01); F02K 9/52 (2006.01); C25B 1/04 (2021.01); C25B 15/08 (2006.01); F02K 9/42 (2006.01); F02K 9/44 (2006.01); F02K 9/95 (2006.01);
U.S. Cl.
CPC ...
F02K 9/64 (2013.01); C25B 1/04 (2013.01); C25B 15/08 (2013.01); F02K 9/425 (2013.01); F02K 9/44 (2013.01); F02K 9/52 (2013.01); F02K 9/68 (2013.01); F02K 9/95 (2013.01); F05D 2220/80 (2013.01); F05D 2240/35 (2013.01); F05D 2260/232 (2013.01); Y02E 60/36 (2013.01);
Abstract
A rocket propulsion system comprises a combustion chamber, a hydrogen-oxygen supply system connected to the combustion chamber, which hydrogen-oxygen supply system is configured to conduct hydrogen and oxygen into the combustion chamber, and a coolant supply system connected to the combustion chamber, which coolant supply system is configured to conduct a combustible coolant into the combustion chamber. An ignition system of the rocket propulsion system is configured to initiate combustion of the hydrogen-oxygen-coolant mixture in the combustion chamber.