|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/322 ; 244/52|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 8 인용 특허 : 4|
An opening in the nose of a missile allows entry of ram air during missile flight to a central chamber. Oppositely oriented steering jets are interconnected with the aft end of the central chamber and escaping ram air provides lateral steering thrust forces. A movable diverting means controls the direction that the escaping ram air is diverted and thereby controls the steering forces.
A system for directionally controlling a fired projectile spinning at a predetermined rate in a predetermined direction when traveling over its flight path comprising: means at the nose end of said projectile for defining a cylindrical chamber having one end open for receiving ram air; a pair of oppositely disposed air passages extending from said chamber means to opposite sides of said projectile; means between said chamber means and said passages for responsively diverting said ram air in a predetermined direction through at least one of said passages ...