|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 3 인용 특허 : 9|
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 innerconnected with the aft end of the central chamber. A diverting mechanism is located between the central chamber and each of the steering jets to allow either one or none of the steering jets to provide correctional steering forces when desired. The rotatable diverting mechanism is pneumatically driven by ram air communicated to an actuation chamber located aft of the valve and controlled by electrically energi...
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 opened for receiving ram air; a pair of oppositely disposed air passages extending from the chamber means to opposite sides of said projectile; means between said chamber means and said passages for blocking ram air flow to both of said passages and for responsively diverting said ram air in a predet...