|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||89/1801 ; 89/1815|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 40 인용 특허 : 2|
An air launched cruise missile carrier airplane having a floor mounted track system for moving missile racks into a launch position adjacent to a side opening in the fuselage and ejecting missiles therethrough, then moving the empty missile racks from the launch location and repositioning a full rack of missiles thereat. A continuous missile launching sequence is provided by the floor track system which guides the movement of the missile racks within a cargo compartment of the fuselage for a continuous carousel movement.
A missile carrier aircraft having an internal missile cargo compartment running along a substantial length of the fuselage, comprising: a track system having a pair of adjacent dual-rail tracks stationarily mounted to the floor of said compartment and running approximately the longitudinal length thereof; said track system having a lateral transfer track terminal at either end of said compartment; said lateral transfer track terminal comprising a section of dual-rail track for shuttling transversely across said compartment and alternately aligning up wit...