• 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Rocket propelled payload with divert control system within nose cone

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/60    F42B-015/01    F42B-010/66    F42B-010/00    F42B-015/00   
미국특허분류(USC) 244/003.22; 244/001R; 244/003.1; 244/003.15; 244/003.21; 244/117R; 244/119; 244/121; 244/158.1; 244/171.7; 244/173.1; 343/872; 102/374; 102/377
출원번호 US-0669935 (2012-11-06)
등록번호 US-9018572 (2015-04-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Cantor Colburn LLP
인용정보 피인용 횟수 : 0  인용 특허 : 21

A rocket is provided and includes booster stages at a rear of the nose cone, the booster stages being configured for propelling the nose cone in a propulsion direction and a divert control system housed entirely in the nose cone for controlling an orientation of the propulsion direction.


1. A rocket, comprising: a nose cone including a payload having a payload attitude control system (ACS);booster stages sequentially disposed at a rear of the nose cone, the booster stages being configured for propelling the nose cone in a propulsion direction; anda divert control system housed entirely in the nose cone for controlling an orientation of the propulsion direction, wherein:the nose cone is configured for ejection from the booster stages once a predefined velocity is attained, andthe payload is configured for ejection from the nose cone follo...

이 특허에 인용된 특허 (21)

  1. Chirivella, Jose E.; VanderWyst, Anton. Active vortex control system (AVOCS) method for isolation of sensitive components from external environments. USP2012048146862.
  2. Kranz Walter (Taufkirchen DEX). Apparatus for correcting the flight path of a missile. USP1987074681283.
  3. Becker Wilfried (Duesseldorf DEX) Grosswendt Werner (Ratingen DEX) Schwenzer Michael (Hermannsburg DEX). Device for guiding a missile. USP1995075433399.
  4. Shiau, Chin; Facciano, Andrew. Digital interface unit (DIU) and method for controlling stages of a multi-stage missle. USP2012018104719.
  5. Andrew E. Turner. Expendable launch vehicle. USP2002036360993.
  6. Arszman Jerrold H. (Huntsville AL). Fire and forget missiles system. USP1985054519315.
  7. Horwath, Tibor G.. Guidance seeker system with optically triggered diverter elements. USP2004076766979.
  8. Metz Pierre (Paris FRX). Guided projectile. USP1993085238204.
  9. Grau, John C.; Fiorellini, Arthur J.; Carr, Raymond E.. Jump correcting projectile system. USP2003106629668.
  10. Facciano, Andrew B.; Moore, Robert T.; Hlavacek, Gregg J.; Do, Michael D.. Methods and apparatus for transferring a fluid. USP2011087989744.
  11. Facciano,Andrew B.; Moore,Robert T.; Parry,James E.; White,John Terry. Missile with multiple nosecones. USP2006087082878.
  12. 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.
  13. Labroche Jean-Paul (St. Aubin FRX) Tonnerre Guy-Andr (Olivet FRX) Wisshaupt Daniel (Orleans FRX). Projectile and process for its use. USP1992065123612.
  14. Bar Klaus (Lauf DEX) Lehrieder Gunther (Rothenbach DEX). Projectile with correctable trajectory. USP1991105054712.
  15. Preston, Kenneth G.; Leal, Michael A.; Wilson, Rondell J.; Hussey, Richard C.. Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control. USP2014058735788.
  16. Morenus Richard C. (Long Beach CA) Frazer Alson C. (Santa Ana CA). Ram air combustion steering system for a guided missile. USP1986034573648.
  17. Bains William R. (Lake Elsinore CA) Sumrall Calhoun W. (Irvine CA). Ram air steering system for a guided missile. USP1985064522357.
  18. Hoever Jeffrey P. (Santa Clara CA) Reginato Richard L. (Sunnyvale CA) Bay Frederic M. (Sunnyvale CA) Rolon Claudia E. (Sunnyvale CA) Bazigos Michael (Belmont CA) Allen Rolla W. (Santa Clara CA). Rocket nozzle snubber. USP1991105060550.
  19. Palathingal, Mohan J.; Grau, John C.. Technique for improving accuracy of high speed projectiles. USP2003056565036.
  20. Kranz Walter (Taufkirchen DEX). Thrust nozzle system. USP1986054589594.
  21. Brown,Charles C.; Beyer,Philip T.. Thrust vectoring a flight vehicle during homing using a multi-pulse motor. USP2006037012233.