|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|인용정보||피인용 횟수 : 10 인용 특허 : 0|
A radial bleed total thrust control system for a rocket propelled missile. In the preferred embodiment, the apparatus employs at least two pairs of straight radial nozzles which are disposed within and penetrate the skin of the missile and at least two pairs of tangentially canted radial nozzles which are also disposed within and penetrate the skin of the missile to provide control moments necessary to control the pitch, yaw, roll and/or the axial thrust of the missile. In one embodiment the radial and tangential nozzles are supplied by the same source o...
A method of controlling a gas propelled body having a main chamber, an axial thrust apparatus and a plurality of radial nozzles, comprising the steps of: (a) generating a propelling gas flow in the main chamber; (b) directing said propelling gas flow to said axial thrust apparatus; (c) selectively diverting at least a portion of said propelling gas flow from said axial thrust apparatus to said plurality of radial control nozzles by selectively and independently opening and closing said radial control nozzles to control the direction and magnitude of the ...