|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/322 ; 60/231 ; 239/26523 ; 239/26517|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 4 인용 특허 : 0|
A control system for providing directional control to a missile during boost phase operation. The kinetic energy of the propellant exhaust gases is utilized to pump a vacuum in an annulus located around the rocket nozzle. To provide a reaction force to guide the missile, a closure is removed from one of several reaction nozzles located around the periphery of the aft end of the rocket and in communication with the vacuum chamber and the atmosphere. A thrust is generated by the air flowing through the reaction nozzle, into the vacuum chamber responsive to...
A directional control system for maintaining a missile on a launch predetermined path comprising: a. a body having forward, intermediate, and aft sections, said intermediate section enclosing a propellant and said aft section enclosing a nozzle in communication with said propellant; b. an annulus chamber carried in said aft section around said nozzle means for creating a vacuum in said chamber comprising an opening at the aft most end thereof whereby the kinetic energy of the burning propellant exhaust gases pump a vacuum in said annulus chamber, said an...