|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F42B-015/00 F42B-013/28 F42B-013/50|
|미국특허분류(USC)||102/489 ; 102/393|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 48 인용 특허 : 6|
Apparatus for deploying one or more submissiles (15) from a carrier missile (25) whereby each submissile (15) is deployed into a flight path which is initially parallel to a streamline (20) of the fluid flow contiguous to the carrier missile (25). An ejection mechanism (45) has a submissile support member (105) oriented substantially parallel to the streamline (20) at the point where the submissile (15) is separated from the support member (105). The ejection mechanism (45) also provides a minimum side force to the submissile (15) which is proportional t...
Apparatus for deploying a body from a stowed position within a moving carrier vehicle to an operative position intially parallel to a high velocity fluid stream contiguous said carrier vehicle, comprising: a deployment assembly provided with an exterior surface covering and being attached to said vehicle, said assembly including means for ejecting at least one body, said ejection means comprising means supporting said body along a longitudinal axis that is oriented substantially parallel to said fluid stream as said body is being ejected; means cooperati...