|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||102/481 ; 60/391 ; 60/223 ; 60/253|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 49 인용 특허 : 0|
A heat sensitive case/nozzle interface is provided for an insensitive propellant-loaded munition such that the interface loses its structural integrity when high external heat is applied. The joint between a rocket case housing a rocket motor and nozzle forming the interface is received by an internal spring retainer positioned in a first groove in the case or nozzle in cooperation with a fusible material housed in an aligned second groove in the nozzle or case, respectively. A plurality of aligned openings extend into said first and second grooves. When...
A munition that loses integrity and separates into component parts when the ambient temperature of an interface mounting means of said munitions exceeds a predetermined temperature comprising: a case having a groove therein; said groove having a plurality of holes spaced radially around and in communication with said groove; a nozzle having a groove therein, said grooves in said case and nozzle being in alignment and forming an interface between the case and nozzle when said case and nozzle are positioned together; a spring retainer positioned in said gr...