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filingDate 2018-07-26-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationDate 2020-09-24-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber JP-2020528519-A
titleOfInvention Space propulsion system
abstract A space propulsion system (1) with a smaller size is specially designed for application to small satellites, but can be easily scaled based on the wide range of sizes of the vehicle of interest, and a space propulsion system (1). ) Is a combustion chamber (10) realized by the cylindrical container (11), and follows the tangential direction of the cylindrical wall (13) and the cylindrical wall so as to guide the spiral combustion path in the combustion chamber (10). A first end (12) provided with at least an injection duct (15) for the combustion agent, fuel, and / or a mixture thereof for injection, and a possible additional vertical injection for the fuel or combustion agent. It has a duct (16) and an opposite end (14) provided with a discharge duct (19) arranged along the tangential direction of the cylindrical wall (13) to receive and direct the spiral path, and is cylindrical. An ultrasonic nozzle connected to a combustion chamber (10) in which the wall has a deposit of catalytic material inside to accelerate the combustion reaction and the above-mentioned discharge duct (19) for discharging combustion products in the combustion chamber. (20) and.
priorityDate 2017-07-28-04:00^^<http://www.w3.org/2001/XMLSchema#date>
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