|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/323 ; 244/324 ; 244/329|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 8 인용 특허 : 3|
An improved missle tail fin assembly. The missile utilizes four tail fin assemblies, each assembly comprising a fitting having three locking portions, each of which comprises a gudgeon having a pair of locking teeth, and a fin having mating recesses for the locking portions. A portion of the material associated with recesses of the two forward locks of each fin is removed, leaving clearances which permit limited rotation about the fin pivot axis in one direction only. When the fin is loaded in a direction to produce clockwise torque, all three locks whic...
The method of compensating for roll rate decay from a predetermined roll rate of a missile having a plurality of tail fins for establishing said predetermined roll rate in flight, each tail fin being mounted to the missile on a pivot axis by at least two longitudinally displaced locking mechanisms that are located respectively forward and rearward of the center of pressure of the fin, each locking mechanism including a plurality of teeth and mating slots limiting the pivotal movement of an associated portion of the fin, the decay of said predetermined ro...