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특허 상세정보

Rocket flight direction control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-015/02   
미국특허분류(USC) 244/52 ; 244/322 ; 60/230 ; 239/26535
출원번호 US-0313891 (1989-02-23)
우선권정보 JP-0038546 (1988-02-23); JP-0021793 (1988-02-23)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 15  인용 특허 : 4
초록

To quickly change rocket flight direction immediately after a rocket has been launched without increasing the wing area, the rocket flight direction control system comprises four steering wings for controlling rocket flight directions; four deflectable nozzles for jetting combustion gas backward to generate rocket thrust; a controller for generating steering control signals; and at least one actuator for actuating the deflectable nozzles in response to the steering control signals in synchronism with steering motion of the steering wings. Further, when t...

대표
청구항

A rocket flight direction control system for a rocket including a rocket body and a combustion chamber, said rocket flight direction control system comprising: (a) steering wing means, pivotally attached to said rocket body, for controlling rocket flight directions; (b) deflectable nozzle means, deflectively attached to said rocket body, for jetting combustion gas from said combustion chamber to generate rocket thrust, said deflectable nozzle means comprising; (1) a fixed divergent nozzle of the overexpansion type, fixedly coupled to said combustion cham...

이 특허를 인용한 특허 피인용횟수: 15

  1. Larsen Richard K. (Lahambra CA). Actuation system with passive compensation for transient loads. USP1997035607123.
  2. Ransom Stephen (Stuhr DEX) Relotius Klaus-Dieter (Bremen DEX). Apparatus for controlling the structural dynamic response of a rocket. USP1997015593110.
  3. Speicher John M. (Geyserville CA) Voigt Allan A. (Geyserville CA) Voigt Che-Ram S. (Geyserville CA). Differential yoke-aerofin thrust vector control system. USP1997055630564.
  4. Teneze, Bernard; Blin, Michel. Flying object for observing the ground. USP2010077763834.
  5. Haight, Stephen D.; Chasman, Daniel; Perez, Juan A.. Hybrid missile propulsion system with reconfigurable multinozzle grid. USP2012028117847.
  6. Danielson, Arnold O.. Integrated aerodynamic fin and stowable TVC vane system. USP1994065320304.
  7. Haag Thomas W.. Ion thruster support and positioning system. USP1998045738308.
  8. Chasman,Daniel B.; Leal,Michael; Haight,Stephen D.. Missile control system and method. USP2007107287725.
  9. Chasman,Daniel; Haight,Stephen D.; Facciano,Andrew B.. Missile control system and method. USP2006097108223.
  10. Corder, David A; Merems, Paul A. Passive stability system for a vehicle moving through a fluid. USP2016089429401.
  11. Chasman, Daniel; Haight, Stephen D.. Propulsion system with canted multinozzle grid. USP2010127856806.
  12. Lane, Jeffery G.; Magarro, Richard B.. Rocket engine nacelle. USP2004076758437.
  13. Cesaroni, Anthony Joseph. Surface skimming munition. USP2015018939084.
  14. Cesaroni, Anthony Joseph. Surface skimming munition. USP2016099448049.
  15. Bernard Marc (Marcilly en Villette FRX). System of vehicle guidance by continuous gas jets. USP1991045004184.