|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/322 ; 244/324 ; 244/58 ; 244/63|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 19 인용 특허 : 5|
A relatively inexpensive, high efficiency, detachable thrust vector mechanism is provided for addressing the current shortcomings in the art. In the illustrative embodiment, the invention is used in conjunction with a nautical or aeronautical vehicle having primary propulsion means and at least one fin movable, to provide maneuverability, in response to a conventional control system. The invention is a detachable thrust vector mechanism comprising auxiliary propulsion means pivotally attached to the missile through connecting means. Contact means are pro...
A detachable thrust vector mechanism for a missile having a primary propulsion means and at least one control fin movable in response to a control system, said detachable thrust vector mechanism comprising: a ring member shaped and adapted for slidable engagement with the aft end of said missile; auxiliary propulsion means pivotally attached to said ring member; and contact means affixed to said auxiliary propulsion means and configured for contacting said at least one control fin whereby bidirectional motion of said fin produces corresponding bidirectio...