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:
Feb. 13, 2024

Filed:

Oct. 20, 2021
Applicant:

Arianegroup Gmbh, Taufkirchen, DE;

Inventor:

Christian Hessel, Taufkirchen, DE;

Assignee:

ArianeGroup GmbH, Taufkirchen, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/40 (2006.01); F02K 9/42 (2006.01); B64G 1/42 (2006.01); F17C 7/02 (2006.01); H01M 8/0656 (2016.01);
U.S. Cl.
CPC ...
B64G 1/401 (2013.01); B64G 1/402 (2013.01); B64G 1/423 (2013.01); F02K 9/425 (2013.01); F17C 7/02 (2013.01); H01M 8/0656 (2013.01); F17C 2205/0332 (2013.01); F17C 2221/011 (2013.01); F17C 2221/012 (2013.01); F17C 2223/0161 (2013.01); F17C 2265/066 (2013.01); F17C 2270/0197 (2013.01); H01M 2250/20 (2013.01);
Abstract

A rocket propulsion system comprising a first cryogenic tank and a second cryogenic tank, wherein the first cryogenic tank is filled with a first propellant, and the second cryogenic tank is filled with a second propellant, for purposes of feeding at least one repeatedly ignitable main propulsion unit in a propulsion phase of the rocket propulsion system. For purposes of tank pressurization via at least a low level of acceleration in a ballistic phase, a first auxiliary propulsion unit can be operated by means of a first gas pressure accumulator, and at least one further auxiliary propulsion unit can be operated by means of a further gas pressure accumulator, and the rocket propulsion system is assigned an energy conversion unit, which is designed at least to charge the first and the second gas pressure accumulator, preferably in the ballistic phase.


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