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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0643799 (1991-01-18) |
발명자 / 주소 |
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인용정보 | 피인용 횟수 : 1 인용 특허 : 0 |
The missiles of the present invention are guided toward the rotating wing aircraft that are their targets by acoustic guidance and control systems that home in on the acoustic signatures of their targets, and that do so despite echoes, the acoustic signatures of other weapons, targets hidden by the
A weapon for attacking a rotating wing aircraft target comprising: (a) means for propelling said weapon toward said aircraft, (b) an acoustic guidance system for guiding said weapon along at least a portion of the path toward the source of the perceived acoustic signature of said target, (c) a warhe
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