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특허 상세정보

Liquid-solid propulsion system and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-009/28    F02K-011/00   
미국특허분류(USC) 60/219 ; 60/251 ; 60/260 ; 60/267
출원번호 US-0541862 (1990-06-21)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 22  인용 특허 : 0
초록

A liquid-solid propulsion system having a tank of liquid oxygen and a high pressure chamber loaded with solid grain fuel with a portion of the liquid oxygen being passed through a heat exchanger to convert the liquid oxygen to gaseous oxygen. The gaseous oxygen is directed to the chamber or solid grain fuel to induce a fuel rich gas burn that is directed to a thrust chamber which also receives liquid oxygen to increase the characteristic velocity of the exhaust and thereby provide the specific impulse of the propulsion system. The gaseous oxygen is also ...

대표
청구항

A liquid-solid propulsion system comprising: A source of liquid oxygen; a source of solid grain fuel; conversion means connected to the source of liquid oxygen and arranged to convert liquid oxygen into gaseous oxygen; first controllable means adapted to introduce a first portion of said gaseous oxygen into the source of solid grain fuel to induce a fuel rich gas burn therewith and to introduce a second portion of said gaseous oxygen back into the source of liquid oxygen whereby said second portion of gaseous oxygen pressurizes said liquid oxygen to prov...

이 특허를 인용한 특허 피인용횟수: 22

  1. Bulman, Melvin J.; Siebenhaar, Adam. Combined cycle missile engine system. USP2011118056319.
  2. Knight, Andrew F.. Cool gas generator and ultra-safe rocket engine. USP2005116968673.
  3. Knuth William H. ; Rice Eric E. ; Kohles Darin R. ; St. Clair Christopher P. ; Gramer Daniel J.. Cryogenic solid hybrid rocket engine and method of propelling a rocket. USP2000086101808.
  4. Oleynik, Vladislav; Ezell, Melvin Jason; Riggs, Jeffrey L.; Albul, Gennadiy. Electrical power generator. USP2012108294287.
  5. Dulligan, Michael; Lake, James; Adkison, Paul; Spanjers, Greg; White, David; Nguyen, Hieu. Electrically controlled extinguishable solid propellant motors. USP2010097788900.
  6. Riggs, Jeffrey L.; Oleynik, Vladislav; Borovikov, Valery; Albul, Gennadiy. Explosive decompression propulsion system. USP2012058181561.
  7. Hayes Michael D.. Fuel strip. USP1998025718113.
  8. Sarigul Klijn,Marti; Sarigul Klijn,Nesrin; Benson,Jim; Williams,Grant; Macklin,Frank. High propulsion mass fraction hybrid propellant system. USP2008077404288.
  9. Grainger,Chris; Macklin,Frank. Hybrid propulsion system. USP2006077069717.
  10. MacKlin,Frank; Grainger,Chris. Hybrid propulsion system. USP2009037503165.
  11. Macklin, Frank; Grainger, Chris. Hybrid propulsion system. USP2012018099945.
  12. Smith Kevin W. ; Kline Korey R. ; Slack ; Jr. Theodore C. ; Mossberg Andrew E.. Hybrid rocket system and integrated motor for use therein. USP1999045893266.
  13. Smith Kevin W. ; Kline Korey R. ; Slack ; Jr. Theodore C.. Hybrid rocket system with disposable cartridge. USP2000016016652.
  14. Kline Korey R. ; Smith Kevin W. ; Bales Thomas O.. Integral solid booster and hybrid thrust sustaining system and projectile incorporating the same. USP2000106125763.
  15. Nelson Steven D. ; Sipes William J. ; Hoffmaster David K.. Mems synthesized divert propulsion system. USP2001016178741.
  16. Dulligan, Michael; Lake, James; Adkison, Paul; Spanjers, Greg; White, David; Nguyen, Hieu. Methods of controlling solid propellant ignition, combustion, and extinguishment. USP2010087770380.
  17. Oleynik, Vladislav; Ezell, Melvin Jason; Riggs, Jeffrey L.; Albul, Gennadiy. Multiphase material generator vehicle. USP2013028378509.
  18. Brian M. Frankie ; Robert M. Zubrin ; Scott E. Lowther. Nitrous oxide based oxygen supply system. USP2002026347627.
  19. Frankie,Brian M.; Zubrin,Robert M.; Lowther,Scott E.. Nitrous oxide based oxygen supply system. USP2007017165546.
  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. Jones H. Stephen. Stable-combustion oxidizer for hybrid rockets. USP2000066073437.
  22. Jones H. Stephen. Stable-combustion oxidizer vaporizer for hybrid rockets. USP1998085794435.