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특허 상세정보

Safe propulsion system for missile divert thrusters and attitude control thrusters and method for use of same

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-009/42   
미국특허분류(USC) 60/204 ; 60/260
출원번호 US-0249429 (1994-05-25)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 15  인용 특허 : 0
초록

A propulsion system for use with a missile or like aerial projectile is disclosed which is suitable for use to operate the divert thrusters and the attitude control thrusters of such a missile while using non-toxic propellants which are entirely non-reactive during storage, transportation, and handling. In the preferred embodiment of the present invention, highly refined liquid hydrocarbon fuel and oxygen gas are used as the propellants, with a relatively small amount of the liquid hydrocarbon fuel and a relatively large amount of the oxygen gas being co...

대표
청구항

A method of igniting fuel fluid in a propulsion system, comprising: a) storing a supply of fuel fluid in a fuel storage tank; b) storing a supply of oxidant fluid in an oxidant storage tank; c) heating the oxidant fluid above the ignition temperature of the fuel fluid in an oxidant heater; and d) supplying heated oxidant fluid from said oxidant heater and said fuel fluid from said fuel storage tank to a combustion chamber wherein said heated oxidant fluid and said fuel fluid impinge to thereby ignite the fuel fluid and produce thrust.

이 특허를 인용한 특허 피인용횟수: 15

  1. Hanlon, Casey; Geck, Kellan; Johnson, Andrew T.. Actuation assembly. USP2012128338768.
  2. Peyrisse, Daniel; Le Louedec, Dominique; Conrardy, Jean-Marie. Bundle comprising two pairs of tanks, and an airborne launcher including such a bundle. USP2012078226045.
  3. Satchell, Jr., Donald Prentice; Feldermann, Christian Juan. Burner and combustion method for the production of flame jet sheets in industrial furnaces. USP2003066579085.
  4. Dulligan, Michael; Lake, James; Adkison, Paul; Spanjers, Greg; White, David; Nguyen, Hieu. Electrically controlled extinguishable solid propellant motors. USP2010097788900.
  5. Henderson, John B.; Goodzeit, Neil E.. Enhanced high-efficiency spacecraft propulsion system. USP2010077762498.
  6. Nelson Steven D. ; Sipes William J. ; Hoffmaster David K.. Mems synthesized divert propulsion system. USP2001016178741.
  7. Menke, Andreas; Burger, Arne; Heberle, Matthias. Method for determining a buffer effect of an activated carbon filter. USP2017029562842.
  8. Dulligan, Michael; Lake, James; Adkison, Paul; Spanjers, Greg; White, David; Nguyen, Hieu. Methods of controlling solid propellant ignition, combustion, and extinguishment. USP2010087770380.
  9. Wood, James Richard. Missile, chemical plasm steering system, and method. USP20181010113844.
  10. 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.
  11. Schneider Steven J.. Reduced toxicity fuel satellite propulsion system. USP2001086272846.
  12. Schneider Steven J.. Reduced toxicity fuel satellite propulsion system including axial thruster and ACS thruster combination. USP2001116311477.
  13. Steven J. Schneider. Reduced toxicity fuel satellite propulsion system including catalytic decomposing element with hydrogen peroxide. USP2002046378291.
  14. Schneider Steven J.. Reduced toxicity fuel satellite propulsion system including fuel cell reformer with alcohols such as methanol. USP2001116314718.
  15. Schneider, Steven J.. Reduced toxicity fuel satellite propulsion system including plasmatron. USP2003046546714.