|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02K-009/12 F02K-009/10 F02K-009/36 F02K-009/16 F02K-009/34|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 35|
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 ...
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...