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. 01, 2025

Filed:

Apr. 01, 2021
Applicant:

Aurora Propulsion Technologies Oy, Espoo, FI;

Inventors:

Pihla Pietikäinen, Espoo, FI;

Jaakko Laitinen, Espoo, FI;

Perttu Yli-Opas, Espoo, FI;

Vili Vilenius, Espoo, FI;

Roope Takala, Espoo, FI;

Pyry Peitso, Espoo, FI;

Janne Sievinen, Espoo, FI;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16K 31/02 (2006.01); B64G 1/40 (2006.01); F02K 9/58 (2006.01); F03H 1/00 (2006.01); F03H 99/00 (2009.01); G05D 7/06 (2006.01); B64G 1/26 (2006.01);
U.S. Cl.
CPC ...
F03H 99/00 (2013.01); B64G 1/401 (2013.01); B64G 1/402 (2013.01); F03H 1/0012 (2013.01); F16K 31/025 (2013.01); G05D 7/0635 (2013.01); B64G 1/26 (2013.01); F02K 9/58 (2013.01); F05D 2300/50212 (2013.01);
Abstract

A thruster assembly, including a switch connected to a power source, a thruster, a propellant tank for storing and pressurising a propellant, and a propellant channel for guiding the propellant to the thruster. The thruster includes a space for receiving the propellant from the propellant channel, an electrically controlled heating element, a thruster body having a first thermal expansion coefficient, a valve component having a second thermal expansion coefficient, which is different than the first thermal expansion coefficient, inside the thruster body, and a nozzle, wherein the valve component includes a sealing surface closing the nozzle in a first temperature, and the electrically controlled heating element in response to actuation of the switch heats said thruster to a second temperature where the thermal expansion of the thruster opens the nozzle.


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