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특허 상세정보

Unitized hybrid rocket system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-009/28    F02K-009/00   
미국특허분류(USC) 060/251; 060/253; 244/171.1
출원번호 UP-0516828 (2004-03-29)
등록번호 US-7540145 (2009-07-01)
국제출원번호 PCT/US04/009694 (2004-03-29)
§371/§102 date 20051101 (20051101)
국제공개번호 WO04/085252 (2004-10-07)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Christie, Parker & Hale, LLP.
인용정보 피인용 횟수 : 4  인용 특허 : 20
초록

The hybrid rocket system of this invention is characterized by use of an oxidizer tank having a cylindrical midsection surrounded by a skirt and bonded thereto by a layer of elastomeric adhesive. The skirt outer surface is in turn adhesively secured to a spacecraft inner surface. An elongated solid-fuel motor case is mechanically rigidly secured to a central rear surface of the tank, and the case terminates in a throat and nozzle. The elastomeric-adhesive bonding of tank to skirt, and rigid adhesion of skirt to spacecraft forms the sole support for the ...

대표
청구항

What is claimed is: 1. In a suborbital spacecraft having a fuselage with a generally central and open interior cylindrical surface, a hybrid-rocket propulsion system, comprising an oxidizer tank having an outer and central cylindrical surface covered by a skirt, and insertable within the fuselage interior surface, the skirt and tank being secured together by an elastomeric means, and an outer surface of the skirt being adhesively secured to the fuselage interior surface; an elongated and generally cylindrical solid-fuel motor case rigidly secured to a c...

이 특허에 인용된 특허 (20)

  1. Floyd, Brian A.. Case burning rocket with drive system for combustion chamber and nozzle. USP2004086782693.
  2. O\Driscoll Peter F. (Los Altos CA). Dome restraint assembly for rocket motors. USP1986034577542.
  3. Bradford Michael D. (Santa Maria CA) McKinney Bevin C. (Ventura CA). Embedded pressurization system for hybrid rocket motor. USP1992065119627.
  4. Smith Kevin W. ; Kline Korey R. ; Slack ; Jr. Theodore C.. Hybrid rocket system and disposable cartridge for use therein. USP2000076082097.
  5. Smith Kevin W. ; Kline Korey R. ; Slack ; Jr. Theodore C. ; Mossberg Andrew E.. Hybrid rocket system and integrated motor for use therein. USP1998025715675.
  6. Smith Kevin W. ; Kline Korey R. ; Slack ; Jr. Theodore C. ; Mossberg Andrew E.. Hybrid rocket system and integrated motor for use therein. USP1999045893266.
  7. Smith Kevin W. ; Kline Korey R. ; Slack ; Jr. Theodore C. ; Mossberg Andrew E.. Hybrid rocket system and integrated motor for use therein. USP2000056058697.
  8. Smith Kevin W. ; Kline Korey R. ; Slack ; Jr. Theodore C. ; Mossberg Andrew E.. Hybrid rocket system and integrated motor for use therein. USP2000076085516.
  9. Smith Kevin W. ; Kline Korey R. ; Slack ; Jr. Theodore C. ; Mossberg Andrew E.. Hybrid rocket system and integrated motor for use therein. USP2000076092366.
  10. Smith Kevin W. ; Kline Korey R. ; Slack ; Jr. Theodore C.. Hybrid rocket system with disposable cartridge. USP2000016016652.
  11. Le Tanter Grard (Castelnau Medoc FRX) Luscan Bernard (Merignac FRX). Integral booster/ramjet drive. USP1986124631916.
  12. Kline Korey R. ; Smith Kevin W. ; Bales Thomas O.. Integral solid booster and hybrid thrust sustaining system and projectile incorporating the same. USP2000106125763.
  13. Zachary R. Taylor. Integrated tankage for propulsion vehicles and the like. USP2002126499287.
  14. Bliley Ward L. (Chesterland OH). Lined pressure vessels. USP1985034504530.
  15. Hoffmeister, Lawrence D.; Madderra, Jimmy M.; Thompson, Richard J.. Liquid fuel expulsion system. USP1985124561568.
  16. Van Name Frederick W. (Newark DE) Gerace Michael A. (Nottingham PA) Singer Victor (Newark DE) Walsh Brendan M. (Wilmington DE). Low cost segmented structure for pressure vessels, rocket motors, piping. USP1994085341638.
  17. Beck Emory J. (Golden CO). Method of manufacturing an overwrapped pressure vessel. USP1976073969812.
  18. Humiston Robert G. (Ogden UT) Ralston Joseph L. (North Ogden UT) Marchant Brent R. (Ogden UT). Reduced cost membrane seal assembly for pulsed rocket motor. USP1997035613358.
  19. Briley Gary L. (Chatsworth CA). Rocket motor containing improved oxidizer injector. USP1992045101623.
  20. Smith Bradley W. (Ogden UT) Youngkeit Dean C. (Willard UT). Solid propellant canister loaded multiple pulsed or staged rocket. USP1991125070691.