|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||89/15 ; E ; 89/1814 ; 89/1815 ; 89/1816|
|우선권정보||DE-2829451 (1978-07-05); DE-2829934 (1978-07-07)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 12 인용 특허 : 0|
The present weapons system enables an aircraft to attack simultaneously a plurality of targets in an aimed, guided manner by a like plurality of small missiles or projectiles. For this purpose the missiles are carried in a rotatable drum type platform comprising respective launching tubes. The firing control system of the aircraft includes a computer which takes into account automatically the target coordinates and other data for selecting that missile which is most suitable for a particular target, whereby the rotatable platform requires a minimum of ro...
An apparatus for the guided attack on multiple targets by means of a weapons carrier combat aircraft, comprising a firing control system including computer means (17) and firing control data input means operatively connected to said computer means, rotary drum means (13, 113) comprising a plurality of rotary drum platforms, housing means (12, 111, 114, 114a) operatively securing said rotary drum means to the underside of said combat aircraft, said housing means comprising firing openings arranged to permit the firing of projectiles substantially in the f...