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특허 상세정보

Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-009/12    F02K-009/10    F02K-009/36    F02K-009/16    F02K-009/34   
미국특허분류(USC) 060/255;
출원번호 US-0195629 (2011-08-01)
등록번호 US-9038368 (2015-05-26)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Sutherland Asbill & Brennan LLP
인용정보 피인용 횟수 : 0  인용 특허 : 35
초록

Certain embodiments of the invention may include systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor. According to an example embodiment of the invention, a method is provided for producing a multi-fuel hybrid motor. The method can include forming a body, where the body includes one or more intake ports; one or more exit nozzles; one or more channels connecting the one or more intake ports with the one or more exit nozzles; and a plurality of cavities comprising segment walls in communication with the one or more channels. The ...

대표
청구항

1. An apparatus comprising: a multi-fuel rocket motor comprising:a body comprising:an intake port; andan exit nozzle;a channel connecting the intake port with the exit nozzle;a turbulator fin extending into the channel connecting the intake port with the exit port;a plurality of cavities comprising one of plastic or rubber segment walls in communication with the channel wherein the segment walls have a first burn consumption rate; anda propellant fuel comprising liquefied paraffin disposed within the plurality of cavities, wherein at least a portion of t...

이 특허에 인용된 특허 (35)

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