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특허 상세정보

Hybrid rocket system and integrated motor for use therein

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-009/72   
미국특허분류(USC) 60/251 ; 60/257
출원번호 US-0383522 (1995-02-03)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Cushman, Darby &Cushman IP Gorup of Pillsbury Madison & Sutro LLP
인용정보 피인용 횟수 : 27  인용 특허 : 0
초록

A hybrid rocket system and motor includes an oxidant tank communicating with a combustion chamber containing a solid fuel grain. The passage from the oxidant tank to the combustion chamber is obstructed by a fill tube which fills the oxidant tank with oxidant and pressurizes it. Once the tank is full, the fill tube is displaced from the tank-chamber passage to deliver oxidant to the grain and initiate the combustion process. The motor may be an integral part of the rocket, or it may be a modular, expendable or exchangeable cartridge-type device inserted ...

대표
청구항

[ What is claimed is:] [1.] A solid/fluid hybrid propulsion system for a projectile launchable from a launch platform, comprising:a container having a fluid reactant therein;a combustion chamber containing a solid reactant therein and having a thrust nozzle at one end thereof;a fluid-flow pathway between said fluid reactant container and said combustion chamber; anda flow-control member which comprises an elongated member of selected length secured to the launch platform and extending through said combustion chamber into said fluid-flow pathway to obstru...

이 특허를 인용한 특허 피인용횟수: 27

  1. Fuller, Jerome K.. Buried radial flow rapid prototyping rocket motors. USP2013128601790.
  2. Dulligan, Michael; Lake, James; Adkison, Paul; Spanjers, Greg; White, David; Nguyen, Hieu. Electrically controlled extinguishable solid propellant motors. USP2010097788900.
  3. Kline, Korey R.; Smith, Kevin W.; Cesaroni, Anthony Joseph. Flame holder for a hybrid rocket motor. USP2004056739121.
  4. Sarigul Klijn,Marti; Sarigul Klijn,Nesrin; Benson,Jim; Williams,Grant; Macklin,Frank. High propulsion mass fraction hybrid propellant system. USP2008077404288.
  5. Karabeyoglu, M. Arif; Altman, David; Cantwell, Brian J.. High regression rate hybrid rocket propellants. USP2004026684624.
  6. Karabeyoglu, M. Arif; Altman, David; Cantwell, Brian J.. High regression rate hybrid rocket propellants and method of selecting. USP2005046880326.
  7. Grainger,Chris; Macklin,Frank. Hybrid propulsion system. USP2006077069717.
  8. MacKlin,Frank; Grainger,Chris. Hybrid propulsion system. USP2009037503165.
  9. Macklin, Frank; Grainger, Chris. Hybrid propulsion system. USP2012018099945.
  10. Kline, Korey R.; Smith, Kevin W.. Hybrid rocket motor having a precombustion chamber. USP2004016679049.
  11. Kline, Korey R.; Smith, Kevin W.. Hybrid rocket motor having a precombustion chamber. USP2004116820412.
  12. Kline, Korey R.; Smith, Kevin W.; Bales, Thomas O.. Hybrid rocket motor using a turbopump to pressurize a liquid propellant constituent. USP2004026684625.
  13. Kline, Korey R.; Smith, Kevin W.; Schmidt, Eric E.; Bales, Thomas O.. Hybrid rocket motor using a turbopump to pressurize a liquid propellant constituent. USP2003116640536.
  14. Brady, Brian Blaise; DeSain, John D. Hypergolic hybrid motor igniter. USP2016039273635.
  15. Kline, Korey R.; Deville, Derek Dee. Ignition systems for hybrid and solid rocket motors. USP2005076912839.
  16. Kline Korey R. ; Smith Kevin W. ; Bales Thomas O.. Integral solid booster and hybrid thrust sustaining system and projectile incorporating the same. USP2000106125763.
  17. Runemard, Mats; Vieider, Christian. Method and device for mixing and initiating a pyrotechnic charge. USP2013128603271.
  18. Dulligan, Michael; Lake, James; Adkison, Paul; Spanjers, Greg; White, David; Nguyen, Hieu. Methods of controlling solid propellant ignition, combustion, and extinguishment. USP2010087770380.
  19. Jacobson Michael D. ; Burgner Gary R.. Multi-ignition controllable solid-propellant gas generator. USP2001066250072.
  20. Kevin W. Smith ; Theodore C. Slack, Jr. ; Korey R. Kline ; Thomas O. Bales, Jr.. Propulsion system containing a mixed-phase propellant and a method for propelling an object with the same. USP2002046367244.
  21. Fuller, Jerome K.. Radial flow rapid prototyping rocket motors. USP2014048707676.
  22. Jones, Ronald D.. Solid fuel grain for a hybrid propulsion system of a rocket and method for manufacturing same. USP2016099453479.
  23. Fuller, Jerome K.. Stereolithographic rocket motor manufacturing method. USP2012078225507.
  24. Fuller, Jerome K.. Stereolithographic rocket motor manufacturing method. USP2014098844133.
  25. Fuller, Jerome Keith. Systems and methods for casting hybrid rocket motor fuel grains. USP2016089429104.
  26. Fuller, Jerome K.. Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor. USP2015059038368.
  27. Rutan, Elbert L.. Unitized hybrid rocket system. USP2009067540145.