|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/321 ; 244/322 ; 244/327 ; 244/117A|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 7 인용 특허 : 0|
The present invention relates to a strut assembly which may be selectively projected and retracted with respect to associated structure of a solid or liquid propellant rocket of missile, with such structure comprising one of, for example, a nozzle thereof or the body thereof. The invention struct may be projected either internally of the nozzle or externally of the missile body, as desired. Projection and retraction of the strut are accomplished through use of fluid actuation means, the fluid mode of means of which comprises coolant which is also directe...
In a projectile having a body and flying through forces supplied by propulsion means having at least one nozzle, a strut mounted on said projectile and movable between a first retracted position and a second extended position by actuator means, and supply means for supplying coolant to said strut through a passageway having an adjustable orifice including a radial port in said strut, the improvement comprising said supply means also supplying said coolant to said actuator means for extending and retracting said strut said adjustable orifice enlarging as ...