|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/322 ; 102/503|
|§371/§102 date||19830120 (19830120)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 11 인용 특허 : 5|
An open-ended diffusion chamber and an adjacent combustion chamber located in the nose of a projectile to receive ram air that ignites a solid fuel material within the combustion chamber. A pair of oppositely disposed lateral steering ports are provided aft of the combustion chamber and are interconnected therewith via a diverting valve that is controllable to selectively divert the escaping combustion gases from the combustion chamber to one or both of the steering ports to thereby change or maintain the trajectory course of the projectile after firing.
A directional steering system for a guided missile comprising: means defining the nose end of said missile; means within said nose means for receiving ram air therein; means within said nose means adjacent said ram air receiving means for providing combustible fuel; means within said nose means defining a combustion chamber wherein ram air ignites said fuel; means within said nose means and aft of said combustion chamber defining lateral thrust steering ports to provide escape paths for combustion gases from said combustion chambers means to the external...