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특허 상세정보

Guidance control system for projectiles

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/01   
미국특허분류(USC) 244/003.22; 244/003.24; 244/003.27; 244/099.5; 102/372; 102/293
출원번호 US-0042087 (2008-03-04)
등록번호 US-8269156 (2012-09-18)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Goodwin Procter LLP
인용정보 피인용 횟수 : 0  인용 특허 : 26

A projectile is guided by employing heat, generated from the aerodynamic heating of a surface of the projectile while the projectile is in flight, to vaporize a material stored within the projectile. The resulting gas is used to guide the projectile.


1. A method for guiding a projectile, comprising: employing heat, generated from the aerodynamic heating of an exterior surface of the projectile while the projectile is in flight, to vaporize a material stored within an inner chamber of the projectile that is adjacent to the exterior surface of the projectile, the exterior surface of the projectile sealing the inner chamber from the external environment surrounding the projectile; andutilizing a gas generated by the vaporization of the material to guide the projectile. 2. The method of claim 1, wherein ...

이 특허에 인용된 특허 (26)

  1. DiCocco,Jack; Prince,Troy; Patel,Mehul; Ng,Tsun Ming Terry. Aircraft and missile afterbody flow control device and method of controlling flow. USP2006077070144.
  2. Kranz Walter (Taufkirchen DEX). Apparatus for correcting the flight path of a missile. USP1987074681283.
  3. Degnan William G. (Huntington CT) Selleck Robert A. (Trumbull CT). Ballistic tolerant hydraulic control actuator and method of fabricating same. USP1981114300439.
  4. Michel Engelhardt. Heat pipe cooling of aircraft skins for infrared radiation matching. USP2002086435454.
  5. Elam,Daryl B.. Inflatable aerodynamic wing and method. USP2007037185851.
  6. Miller Robert C. (Encino CA) Seemann Rudolf J. (Santa Ana CA). Infrared signature reduction of aerodynamic surfaces. USP1991024991797.
  7. Bulman,Melvin J.; Billig,Frederick S.. Integrated air inlet system for multi-propulsion aircraft engines. USP2007057216474.
  8. Navarette Carlos A. (Canoga Park CA). Linear hydraulic actuator having ballistic tolerant. USP1986094608912.
  9. Cox,Brian Nelson; Davis,Janet B.; Mack,Julia; Marshall,David Bruce; Morgan,Peter E.; Sudre,Olivier H.. Materials for self-transpiring hot skins for hypersonic vehicles or reusable space vehicles. USP2007107281688.
  10. Frey Thomas J. ; Dara Philip H. ; Gerace Michael A. ; Solberg Mark A.. Missile diverter integration method and system. USP1998055755401.
  11. Scott Douglas R. (Knoxville TN). Pneumatic control system and parts therefor and methods of making the same. USP1981054267968.
  12. Smith James M. (Fanibel Island FL). Pneumatic gear motor application. USP1977104052024.
  13. Pinson George T. (Huntsville AL). Pressure gas supply for a missile and the like. USP1987084684080.
  14. Billig Frederick S. (Rockville MD). Propellant utilization system. USP1992085135184.
  15. Robert C. Michelson. Reciprocating chemical muscle(RCM) and method for using same. USP2002096446909.
  16. Schneider Edward T. (8729 Hilltop Mentor OH 44060). Remote controlled high force actuator. USP1991065025627.
  17. Eldridge, Jerome M.. Small scale actuators and methods for their formation and use. USP2005086935355.
  18. Andrew Perrucci. Solid propellant gas generator impulse management scheme for high mass flow turn-down ratio. USP2002076412275.
  19. Goddard Charles W. (San Jose CA) Lucas John T. (Los Altos CA) Galvan Paul A. (San Jose CA). Solid-propellant-powered maneuvering system for spacecraft. USP1991115062593.
  20. Crepin Roger (Paris FRX). Steering arrangement for projectiles of the missile kind, and projectiles fitted with this arrangement. USP1980074211378.
  21. Raynaud Jacques (Savigny-sur-Orge FRX) Darmois Jean (Bourg-la-Reine FRX) Jolivet Pierre (Arcueil FRX) Guillot Jean (Chatenay-Malabry FRX). System for piloting a missile by means of lateral gaseous jets and missile comprising such a system. USP1985074531693.
  22. Morgand Jean-Pierre (Paris FRX). System for steering a missile by means of lateral gas jets. USP1992065123611.
  23. Morgand Jean-Pierre (Paris FRX). System for steering a missile by means of lateral nozzles. USP1991125074492.
  24. Le Touche Roger (Ecquevilly FRX). Thermal protection device using the vaporization and superheating of a rechargeable liquid. USP1994075330124.
  25. Fujita,Toshiharu; Hidaka,Shozo. Three-axis attitude control propulsion device and flying object comprising the same. USP2006097102113.
  26. Tapscott Robert E.. Tropodegradable bromine-containing halocarbon additives to decrease flammability of refrigerants foam blowing agents solvents aerosol propellants and sterilants. USP2001106300378.