System and method for dispensing of multiple kill vehicles using an integrated multiple kill vehicle payload
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F42B-015/01
F41G-009/00
B64D-007/08
F42B-015/00
B64D-007/00
출원번호
US-0923707
(2010-10-05)
등록번호
US-8575526
(2013-11-05)
발명자
/ 주소
Colvin, Randy D.
Wuerl, Adam M.
Mak, Michael S.
출원인 / 주소
Lockheed Martin Corporation
대리인 / 주소
Buchanan Ingersoll & Rooney PC
인용정보
피인용 횟수 :
6인용 특허 :
14
초록▼
An interceptor system and method for dispensing of multiple kill vehicles, including, a carrier vehicle having a central carrier vehicle axis and axial propulsion integrated into the carrier vehicle, a payload adapter associated with the carrier vehicle for connecting a payload to a boost vehicle, t
An interceptor system and method for dispensing of multiple kill vehicles, including, a carrier vehicle having a central carrier vehicle axis and axial propulsion integrated into the carrier vehicle, a payload adapter associated with the carrier vehicle for connecting a payload to a boost vehicle, the payload adapter being located aft of the carrier vehicle, and multiple kill vehicles mounted to the carrier vehicle radially around a circumference of the carrier vehicle.
대표청구항▼
1. An interceptor system for dispensing of multiple kill vehicles, comprising: a carrier vehicle having a central carrier vehicle axis and axial propulsion integrated into the carrier vehicle;a payload adapter associated with the carrier vehicle for connecting a payload to a boost vehicle, the paylo
1. An interceptor system for dispensing of multiple kill vehicles, comprising: a carrier vehicle having a central carrier vehicle axis and axial propulsion integrated into the carrier vehicle;a payload adapter associated with the carrier vehicle for connecting a payload to a boost vehicle, the payload adapter being located aft of the carrier vehicle; andmultiple kill vehicles mounted to the carrier vehicle radially around a circumference of the carrier vehicle. 2. The interceptor system of claim 1, wherein the carrier vehicle, the payload adapter, and the kill vehicles constitute an integrated payload. 3. The interceptor system of claim 2, wherein the integrated payload comprises: an engagement management controller for managing engagement of the kill vehicles with the threat. 4. The interceptor system of claim 3, wherein the engagement management controller is an on-board guidance controller for guiding the interceptor system and wherein the carrier vehicle comprises: an on-board sensor device for sensing a threat to be engaged; anda guidance controller for guiding the payload system. 5. The interceptor system of claim 3, wherein the engagement management controller comprises: a software module for allocating propulsion resources of the integrated payload among: (1) a boost function for extending range of the integrated payload; and (2) a payload mission for guiding the integrated payload to intercept the threats. 6. The interceptor system of claim 3, wherein the engagement management controller comprises: a software module for controlling propulsion resources of the integrated payload for guiding the integrated payload for the kill vehicles to intercept multiple threats. 7. The interceptor system of claim 3, wherein the engagement management controller comprises: a software module for commanding a dispensing of the kill vehicles, and for controlling guidance of the kill vehicles which have been dispensed. 8. The interceptor system of claim 3, wherein the engagement management controller comprises: a software module for controlling communication with kill vehicles which have been dispensed by the integrated payload. 9. The interceptor system of claim 8, wherein the software module maintains communication with a dispensed kill vehicle up to and after a time of predicted intercept when the dispensed kill vehicle is expected to intercept the threats. 10. The interceptor system of claim 1, wherein the propulsion comprises: at least one fuel tank, the kill vehicles being mounted to the carrier vehicle about the fuel tank. 11. The interceptor system of claim 1, wherein the payload comprises: a mono-propellant thruster;a hydrazine fuel tank; anda helium pressurant tank. 12. The interceptor system of claim 11, wherein the payload comprises: multiple mono-propellant thrusters. 13. The interceptor system of claim 1, wherein the payload comprises: a bi-propellant thruster;a monomethylhydrazine (MMH) fuel tank;an oxidizer tank; anda helium pressurant tank. 14. The interceptor system of claim 1, wherein the kill vehicles each comprise: a kill vehicle with mono-propellant for kill vehicle propulsion upon being dispensed from the carrier vehicle. 15. Method for controlling a payload for dispensing of multiple kill vehicles, the method comprising: controlling propulsion of a carrier vehicle, wherein multiple kill vehicles are attached to the carrier vehicle; andmanaging engagement of the kill vehicles with a threat using on-board guidance of the carrier vehicle, on-board kill vehicle guidance, and allocating propulsion resources among extending range of the carrier vehicle, and guiding the carrier vehicle to provide for kill vehicle intercept of a threat based on a controlled dispensing of the kill vehicles. 16. The method according to claim 15, wherein the managing of engagement of the threats comprises: controlling propulsion resources of an integrated payload containing the carrier vehicle and the kill vehicles for guiding the integrated payload to intercept multiple threats. 17. The method according to claim 15, wherein the managing of engagement of the threat comprises: commanding and dispensing of the kill vehicles; andcontrolling guidance of the kill vehicles which have been dispensed using on-board engagement management of the carrier vehicle. 18. The method according to claim 15, wherein the managing engagement of the threat comprises: controlling communication with kill vehicles which have been dispensed using on-board communications of the carrier vehicle. 19. The method according to claim 15, comprising: mounting the kill vehicles about a fuel tank of the carrier vehicle. 20. The method according to claim 15, comprising: propelling a kill vehicle which has been dispensed from the carrier vehicle using a mono-propellant kill vehicle propulsion.
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이 특허에 인용된 특허 (14)
O'Dwyer, James Michael, Directional control of missiles.
Williams,Darin S; Pflibsen,Kent P.; Crawford,Thomas M., Multiple kill vehicle (MKV) interceptor and method for intercepting exo and endo-atmospheric targets.
Morris Joseph W. (Rancho Cordova CA) Carlson Russell W. (Folsom CA) Peterson Kevin L. (Sacramento CA) Reich Edward M. (Orangevale CA), Multiple pintle nozzle propulsion control system.
Sharpin, David; Kolanek, Jim; Cvetnic, Mark A.; Hutchings, Mike; Tennison, James; Nelson, Kent Carl; Hunsberger, Harold Kregg; Baseghi, Behshad, Methods and apparatuses for active protection from aerial threats.
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