IPC분류정보
| 국가/구분 |
United States(US) Patent
등록
|
| 국제특허분류(IPC7판) |
|
| 출원번호 |
US-0284875
(1994-08-02)
|
|
발명자
/ 주소 |
- Sun John (Thousand Oaks CA) Sanders Ross J. (Newbury Park CA) Starace Ralph C. (Camarillo CA) Hackman William K. (Thousand Oaks CA)
|
| 출원인 / 주소 |
- Northrop Grumman Corporation (Los Angeles CA 02)
|
| 인용정보 |
피인용 횟수 :
50 인용 특허 :
0 |
초록
▼
An air defense missile weapon system in which a plurality of unmanned missiles penetrate, survey, identify, attack and destroy target areas that include air defense sites and sites of military interest. Each of the missiles has an airframe, sensors, data links, propulsion means, and a plurality of c
An air defense missile weapon system in which a plurality of unmanned missiles penetrate, survey, identify, attack and destroy target areas that include air defense sites and sites of military interest. Each of the missiles has an airframe, sensors, data links, propulsion means, and a plurality of control surfaces. The missiles are launched from a carrier aircraft towards the target sites from a stand-off range. The missiles preferably operate in cooperative teams of hunter and killer missiles, and are interoperable with a plurality of military aircraft and other existing weapon systems.
대표청구항
▼
A method of destroying a military target site, comprising the steps of: launching a plurality of missiles from an aircraft at a stand-off range from a target area, each said missile having an airframe, means for propulsion of said missile, and control surfaces, at least one of said missiles being a
A method of destroying a military target site, comprising the steps of: launching a plurality of missiles from an aircraft at a stand-off range from a target area, each said missile having an airframe, means for propulsion of said missile, and control surfaces, at least one of said missiles being a hunter missile adapted to include a radio frequency direction finder, an imaging infrared seeker system with automatic target cuing algorithms, an on-board Global Positioning System locating system, a jam-resistant data link system for transmitting and receiving data between said hunter missile and said aircraft and between said hunter missile and other command and control platforms and receiving stations, a radar cross section augmentation system, a laser target designator, and a warhead, at least one of said missiles being a killer missile adapted to include an on-board Global Positioning System locating system, a radar cross section augmentation system, a laser tracker, a jam-resistant data link receiver, and a warhead; deploying said plurality of missiles to said target area; operating said radar cross section augmentation system of at least one of said plurality of missiles to induce emissions of radio frequency energy from said military target site; operating said radio frequency direction finder and said automatic target cuing algorithms of said imaging infrared seeker system of said hunter missile to survey, locate and select a target of said military target site for destruction; directing a selected one of said killer missiles to said selected target; and, detonating said warhead at said selected target.
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