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특허 상세정보

Integral solid booster and hybrid thrust sustaining system and projectile incorporating the same

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/10    C06B-045/00   
미국특허분류(USC) 10/2381 ; 10/228.7 ; 10/229.1 ; 10/234.9 ; 10/235.2 ; 10/237.4 ; 10/220.27 ; 10/227.56 ; 602/53 ; 602/59
출원번호 US-0134322 (1998-08-14)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Gordon
인용정보 피인용 횟수 : 18  인용 특허 : 13
초록

A rocket according to the invention includes a motor having a fuel chamber and an oxidizer tank, a nose portion provided forward of the motor, and a nozzle surrounded by fins provided aft of the motor. The fuel chamber is provided with a relatively central solid propellant, and a hybrid fuel surrounds the solid propellant. The oxidizer tank is filled with a reactant and coupled to the forward end of the fuel chamber. A pathway is provided between the tank and the fuel chamber for the passage of reactant therethrough. At least one of a valve and a barrier...

대표
청구항

[ What is claimed is:] [1.] A propulsion system for a projectile, comprising:a) a fuel chamber having a forward end and provided with a solid propellant and a solid fuel about said solid propellant, said solid propellant provided with a central channel;b) a container for storing a fluid reactant therein, said container coupled to said forward end of said fluid chamber;c) a pathway between said fuel chamber and said container; andd) pathway blocking means for blocking said pathway until said solid propellant is at least partially consumed, and thereafter ...

이 특허에 인용된 특허 (13)

  1. Holzman Allen L. (Cupertino CA). Constant thrust hybrid rocket motor. USP1984014424679.
  2. Bradford Michael D. (Santa Maria CA) McKinney Bevin C. (Ventura CA). Embedded pressurization system for hybrid rocket motor. USP1992065119627.
  3. Barker James M. (P.O. Box 42800 Houston TX 77242-8044). Exploding foil initiator using a thermally stable secondary explosive. USP1995075431104.
  4. Knuth William H. (Huntsville AL) Beveridge John H. (Huntsville AL). Gas-fed hybrid propulsion system. USP1991045010730.
  5. Jones H. Stephen. Hybrid helium heater pressurization system and electrical ignition system for pressure-fed hybrid rockets. USP1998035722232.
  6. Smith Kevin W. ; Kline Korey R. ; Slack ; Jr. Theodore C. ; Mossberg Andrew E.. Hybrid rocket system and integrated motor for use therein. USP1998025715675.
  7. Schuler Alan L. (San Diego CA) Wiley Danny R. (Escondido CA). Liquid-solid propulsion system and method. USP1992035099645.
  8. Rosenfield Gary C. (Las Vegas NV). Pyrotechnic valve, igniter and combustion preheater for hybrid rocket motors. USP1996125579636.
  9. Miskelly ; Jr. Hermann L. (Huntsville AL) Alldredge R. Lance (Arab AL) Owens Thomas F. (Huntsville AL). Pyrotechnically driven nozzle restrictor. USP1995075435128.
  10. Briley Gary L. (Chatsworth CA). Rocket motor containing improved oxidizer injector. USP1992045101623.
  11. Rider Todd (501 W. “A”St. North Little Rock AR 72116). Rocket staging system. USP1988024723736.
  12. Meffert Wolfgang (Dsseldorf DEX) Silligmann Kalr-Heinz (Dsseldorf DEX) Fischer Siegmar (Dsseldorf DEX) Hahn Ulf (Ratingen DEX). Seal for the nozzle opening of a projectile. USP1990064930420.
  13. Burns Bruce P. (Churchville MD) Kirkendall Richard D. (Havre de Grace MD). Solid propellant-carrying caboted projectile. USP1990064936220.

이 특허를 인용한 특허 피인용횟수: 18

  1. Fuller, Jerome K.. Buried radial flow rapid prototyping rocket motors. USP2013128601790.
  2. Maier, Thomas. Control and/or drive device for a flying body. USP2010057707820.
  3. Maier, Thomas. Control and/or drive device for a flying body. USP2012088245496.
  4. Dulligan, Michael; Lake, James; Adkison, Paul; Spanjers, Greg; White, David; Nguyen, Hieu. Electrically controlled extinguishable solid propellant motors. USP2010097788900.
  5. Dawley, Scott K.; Friedlander, III, Mark Peyser. End-burning propellant grain with area-enhanced burning surface. USP2015079079807.
  6. Vickery, Charles A.; Kruse, William D.; Olmos, Mark. External system and method for rocket exhaust plume signature tailoring. USP2003126655124.
  7. Kline, Korey R.; Smith, Kevin W.; Cesaroni, Anthony Joseph. Flame holder for a hybrid rocket motor. USP2004056739121.
  8. Ho, Sook Ying. Hybrid rocket system with moveable combustion control member. USP2013038387361.
  9. Dulligan, Michael; Lake, James; Adkison, Paul; Spanjers, Greg; White, David; Nguyen, Hieu. Methods of controlling solid propellant ignition, combustion, and extinguishment. USP2010087770380.
  10. Fuller, Jerome K.. Radial flow rapid prototyping rocket motors. USP2014048707676.
  11. Vickery, Charles A.; Mason, Jerry N.; Kruse, William D.; Olmos, Mark. Rocket exhaust plume signature tailoring. USP2004026684622.
  12. Jones, Ronald D.. Solid fuel grain for a hybrid propulsion system of a rocket and method for manufacturing same. USP2016099453479.
  13. Dupont, James H.; Loehr, Richard D.; Renz, Robert N.. Solid propellant rocket motor with notched annular fuel. USP2012058181444.
  14. Fuller, Jerome K.. Stereolithographic rocket motor manufacturing method. USP2012078225507.
  15. Fuller, Jerome K.. Stereolithographic rocket motor manufacturing method. USP2014098844133.
  16. Fuller, Jerome Keith. Systems and methods for casting hybrid rocket motor fuel grains. USP2016089429104.
  17. Fuller, Jerome K.. Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor. USP2015059038368.
  18. Rutan, Elbert L.. Unitized hybrid rocket system. USP2009067540145.