Mobile ballistic missile detection and defense system
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F41G-007/00
F42B-015/01
출원번호
US-0375746
(2003-02-26)
발명자
/ 주소
Redano, Richard T.
인용정보
피인용 횟수 :
15인용 특허 :
16
초록▼
The present invention is directed towards a ballistic missile detection and defense system. The system of the present invention comprises a ship based interceptor or antiballistic missile, a missile launch detection system, a missile tracking system, and a ship based signal processing system capable
The present invention is directed towards a ballistic missile detection and defense system. The system of the present invention comprises a ship based interceptor or antiballistic missile, a missile launch detection system, a missile tracking system, and a ship based signal processing system capable of receiving said tracking signal calculating an intercept trajectory for an antiballistic missile to intercept a ballistic missile, and further capable of outputting an intercept trajectory program to an antiballistic missile.
대표청구항▼
The present invention is directed towards a ballistic missile detection and defense system. The system of the present invention comprises a ship based interceptor or antiballistic missile, a missile launch detection system, a missile tracking system, and a ship based signal processing system capable
The present invention is directed towards a ballistic missile detection and defense system. The system of the present invention comprises a ship based interceptor or antiballistic missile, a missile launch detection system, a missile tracking system, and a ship based signal processing system capable of receiving said tracking signal calculating an intercept trajectory for an antiballistic missile to intercept a ballistic missile, and further capable of outputting an intercept trajectory program to an antiballistic missile. cally sealed to a portion of the body inner surface, the first and second strips being located between the first working surface of the first piston and the second working surface of the second piston.7. The fuel injector of claim 3, wherein the first piston includes a piston skirt extending from the first outer surface along the longitudinal axis, the piston skirt including an outer shell and an inner shell, the inner shell being coupled to the extension portion.8. The fuel injector of claim 7, wherein the second piston comprises an annulus having a first surface and a second surface extending along the longitudinal axis, the first surface of the annulus facing the extension portion, the second surface facing the outer shell of the piston skirt, the annulus reciprocable into and out of the outer shell of the piston skirt.9. The fuel injector of claim 8, wherein the flexible fluid barrier comprises a member having a first end coupled to the outer shell of the piston skirt and a second end coupled to an end cap portion, the end cap portion extending from the inner surface of the body towards the longitudinal axis.10. The fuel injector of claim 3, wherein the first piston comprises a plurality of pockets disposed on the first outer surface of the first piston about the longitudinal axis.11. The fuel injector of claim 10, wherein the valve comprises a plate, wherein the plate includes a plurality of orifices formed thereon, and the plate is exposed to the first fluid reservoir such that the plate projects over one of the first and second outer surfaces and whose thickness is approximately {fraction (1/94)} of the square root of the surface area of one side of the plate.12. The fuel injector of claim 11, wherein the plate includes a plurality of orifices disposed in a confronting arrangement with the plurality of pockets on the first outer surface of the first piston.13. The fuel injector of claim 1, wherein the first piston comprises an exterior first piston surface contiguous to the body inner surface so as to permit leakage of hydraulic fluid between the first and second fluid reservoirs.14. A hydraulic compensator for a length-changing actuator, the length-changing actuator having first and second ends, the hydraulic compensator comprising: an end member; a body having a first body end and a second body end extending along a longitudinal axis, the body having an inner surface facing the longitudinal axis;a first piston coupled to the length-changing actuator and disposed in the body proximate one of the first body end and second body end, the first piston having a first outer surface and a first working surface distal to the first outer surface, the first outer surface cooperating with the end member of the housing of the fuel injector to define a first fluid reservoir in the body;a second piston disposed in the body proximate the first piston, the second piston having a second outer surface distal to a second working surface confronting the first working surface of the first piston;a second fluid reservoir disposed between the first working surface and the second working surface;a communication passage disposed between the first fluid reservoir and the second fluid reservoir; andan extension portion coupled to one of the first piston and second piston, the extension portion including a fill passage disposed within the extension portion so as to supply hydraulic fluid to the communication passage and the first and second fluid reservoirs.15. The compensator of claim 14, further comprising a valve disposed in one of the first and second reservoir, the valve being responsive to one of a first fluid pressure in the first fluid reservoir and a second fluid pressure in the second reservoir so as to permit fluid flow from one of the first and second fluid reservoirs to the other of the first and second fluid reservoirs.16. The compensator of claim 14, wherein the second piston comprises an annulus disposed about the longitudinal
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이 특허에 인용된 특허 (16)
Guelman Moshe (Haifa ILX) Yavnai Arie (Kiryat Bialik ILX), Active defense system against tactical ballistic missiles.
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