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특허 상세정보

Integrated propulsion and attitude control system from a common pressure vessel for an interceptor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/66    F42B-015/01    F42B-010/00    F42B-015/00   
미국특허분류(USC) 244/003.22; 244/003.1; 244/003.15; 244/003.21; 244/003.24
출원번호 US-0551221 (2012-07-17)
등록번호 US-8975565 (2015-03-10)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Gifford, Eric A.
인용정보 피인용 횟수 : 0  인용 특허 : 11
초록

An interceptor is provided with an integrated propulsion and attitude control system (ACS) in which propellant burn forms a common pressure vessel for high-pressure gas. An aft port in the rocket motor directs gas through one or more main nozzles that expel high-velocity gas in a generally axial direction to propel the interceptor. A forward port directs gas through one or more attitude control nozzles that expel high-velocity gas in a generally radial direction to control the attitude of the interceptor. The main nozzle(s) and stabilization fins are fix...

대표
청구항

1. An interceptor, comprising: an airframe;a plurality of fixed aerodynamic stabilization fins on the airframe;a rocket motor within the airframe, said motor comprising a motor can having ports forward and aft and a rocket propellant therein, wherein propellant burn forms a common pressure vessel for high-pressure gas;one or more fixed main nozzles having a throat in communication with the aft port and the common pressure vessel to convert high-pressure gas into a first high-velocity gas and expel the first high-velocity gas in a generally axial directio...

이 특허에 인용된 특허 (11)

  1. Ryan William F. (Phoenix AZ). Fluidic thruster control and method. USP1983114413795.
  2. Rolf E. Hamke ; Eric M. Rohrbaugh. Hybrid rocket propulsion system including array of hybrid or fluid attitude-control rocket engines. USP2002056393830.
  3. Gundel, Bernd; Graf, Hans-Rainer; Hammer, Helmut; Thurner, Günther. Method and device for varying a flight path of a projectile by intentional tumbling of the projectile. USP2010067741588.
  4. 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.
  5. Keigler John Edward (Princeton NJ) Muhlfelder Ludwig (Livingston NJ) Cenker Robert Joseph (Princeton NJ). Orientation system for a spin stabilized spacecraft. USP1976083977633.
  6. Metz Pierre (Paris FRX). Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing th. USP1983104408735.
  7. Tubeuf Jean (Le Chesnay FR). Projectile guidance. USP1976083977629.
  8. Unterstein Klaus (Dsseldorf DEX). Projectile steering block. USP1988024726544.
  9. Onojima, Noboru; Tezuka, Hitoshi; Osada, Akira; Yamaguchi, Ichiro. Side thruster of flying object. USP2003016502384.
  10. Morgand Jean-Pierre (Paris FRX). System for steering a missile by means of lateral gas jets. USP1992065123611.
  11. Smith Gregory H. ; Clark Roland D.. Universal driver circuit for actuating both valves and ordnances. USP2001076267326.