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특허 상세정보

Missile control system and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/66    F42B-010/00    F02K-009/80    F02K-009/00   
미국특허분류(USC) 244/003.22; 244/003.1; 244/003.15; 244/003.21
출원번호 US-0289651 (2002-11-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Renner, Otto, Boisselle &
인용정보 피인용 횟수 : 4  인용 특허 : 15
초록

A missile includes a tail section having a multi-nozzle grid with both fixed nozzlettes, and movable, thrust vector nozzlettes. The movable nozzlettes may be configured in a number of discrete array bars, each containing multiple of the movable nozzlettes. Movement of one or more array bars may be used to vector the thrust of the missile, providing roll, yaw, or spinning of the missile, for example.

대표
청구항

What is claimed is: 1. A missile comprising: a nozzle grid including: a plurality of fixed nozzles; and a plurality of movable nozzles; and a pressurized gas source operatively coupled to the nozzle grid; wherein the movable nozzles are divided up into plural separately-actuatable arrays; and wherein the movable nozzles of each of the arrays are in a separate array bar. 2. The missile of claim 1, wherein the missile includes four array bars. 3. The missile of claim 1, wherein the array bars are axisymmetrically spaced about an axis of the mi...

이 특허에 인용된 특허 (15)

  1. East ; George F. ; Hallum ; Charles E.. Combined warm gas fin and reaction control servo. USP1978044085909.
  2. Speicher John M. (Geyserville CA) Voigt Allan A. (Geyserville CA) Voigt Che-Ram S. (Geyserville CA). Differential yoke-aerofin thrust vector control system. USP1996045505408.
  3. McCorkle ; Jr. William C. (Huntsville AL). Directional control system for artillery missiles. USP1977054023749.
  4. Porter Lane (Jupiter FL) Thayer Edward B. (Palm Beach Gardens FL). Hexagonal cluster nozzle for a rocket engine. USP1994095343698.
  5. Young Robert W. (Luton GB2). Jet propulsion efflux outlets. USP1984024432512.
  6. Voigt Che-Ram S. (Geyserville CA). Mechanism for thrust vector control using multiple nozzles. USP1997095662290.
  7. Voigt Allan A. ; Schroeder Richard W. ; Voigt Che-Ram S. ; Speicher John M.. Mechanism for thrust vector control using multiple nozzles and only two yoke plates. USP1999035887821.
  8. Fenton George H. A. (Stevenage GBX) Dransfield Alfred E. (Stevenage GBX). Missiles. USP1988054745861.
  9. 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. USP1995105456425.
  10. Faupell Lawrence C. (Logan UT) Wassom Steven R. (Smithfield UT). Reduced fin span thrust vector controlled pulsed tactical missile. USP1989094867393.
  11. Kubota Naminosuke (Yokohama JPX) Yano Yutaka (Tokyo JPX) Takagi Yasumasa (Higashimatuyama JPX) Ninomiya Kazuyoshi (Tokyo JPX) Shimoguti Nobuo (Tokyo JPX) Terashima Mituhiko (Tokorozawa JPX) Nakano To. Rocket flight direction control system. USP1990044913379.
  12. Seeger Hans-Jochen (Ganderkesee DEX). Steering of an aerodynamic vehicle. USP1979084163534.
  13. Rotmans ; Richard J.. Thrust vector control actuation system. USP1978124131246.
  14. Bennett James (Stevenage GBX) Heath Martin R. (Stevenage GBX) Foulsham Peter G. (Stevenage GBX). Thruster system. USP1989054826104.
  15. Faupell Lawrence C. (North Logan UT) Wassom Steven R. (Smithfield UT) Kliger Joseph J. (North Ogden UT). Vectorable nozzle having jet vanes. USP1996045511745.