$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"
쳇봇 이모티콘
안녕하세요!
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

특허 상세정보

Pellet-loaded multiple impulse rocket motor

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-009/28    F02K-009/00   
미국특허분류(USC) 060/250; 060/253; 060/254; 060/256
출원번호 US-0391216 (2009-02-23)
등록번호 US-8667776 (2014-03-11)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Renner, Otto, Boisselle & Sklar, LLP
인용정보 피인용 횟수 : 0  인용 특허 : 39
초록

There is disclosed an apparatus which may include a common nozzle and a plurality of combustion chambers coupled to the nozzle. Each of the plurality of combustion chambers may include a case, a solid fuel propellant charge in the form of a plurality of fuel pellets, and an igniter disposed to ignite the propellant charge. Each of the plurality of combustion chambers may also include a pellet retainer disposed to retain unignited fuel pellets within the case and a burst disk disposed between the propellant charge and the nozzle. Each burst disk may adapt...

대표
청구항

1. A rocket motor, comprising: a nozzle having a variable cross-sectional area, with a throat of the nozzle being at a smallest cross-sectional area;a plurality of combustion chambers directly coupled to the nozzle, each of the plurality of combustion chambers comprising:a case, with different of the combustion chambers having different cases;a propellant charge comprising a plurality of fuel pellets disposed within the case;an igniter disposed to ignite the propellant charge;a pellet retainer disposed to retain unignited fuel pellets within the case and...

이 특허에 인용된 특허 (39)

  1. Rotkopf, Menachem. Armor piercing projectile. USP2004066745696.
  2. Jones ; Roy A. ; Mabry ; Marshall W.. Barrier system for dual-pulse rocket motor. USP1978044085584.
  3. Granger Charles C. (1203 Chestnut St. Henderson NC 27536). Combustion gas pressure generator. USP1976113992877.
  4. Zheng,Rong; Rho,Hongsang; Yamarte,Luis; Kovacik,Gary J.; Sarkar,Partha. Controlling solid oxide fuel cell operation. USP2007087258936.
  5. Barnes Michael W. (Brigham City UT) Taylor Robert D. (Hyrum UT). Gas generant compositions containing amine nitrates plus basic copper (II) nitrate and/or cobalt(III) triammine trinitra. USP1997035608183.
  6. Daniel W. Doll ; Gary K. Lund ; Craig D. Hughes ; Marc A. Hall ; David J. Macon. Gas generating eject motor. USP2002036352030.
  7. Nakashima, Yoshihiro; Ohji, Nobuyuki. Gas generator for air bag and air bag apparatus. USP2003076598901.
  8. Hinrichs James O. (Odessa MO). High reverse pressure resistant low forward burst pressure rupture disc assembly. USP1985034505180.
  9. Osofsky Irving B. (28327 San Nicolas Dr. Rancho Palos Verdes CA 90274). High velocity impulse rocket. USP1995085440993.
  10. Stevens, George L.. Igniter pellet cup. USP1985094539910.
  11. Linick James (Naples FL). Method and apparatus for radial thrust trajectory correction of a ballistic projectile. USP1997075647558.
  12. Dryer, Richard. Methods and apparatus for projectile guidance. USP2011057947938.
  13. Frey Thomas J. ; Dara Philip H. ; Gerace Michael A. ; Solberg Mark A.. Missile diverter integration method and system. USP1998055755401.
  14. Woessner, George T.. Missile thrust system and valve with refractory piston cylinder. USP2005056895991.
  15. Lundstrom Norman H.. Monopropellant and propellant compositions including mono and polyaminoguanidine dinitrate. USP2000046045638.
  16. Bastian Thomas W. (Fullerton CA) Roberts J. Sydney (Fullerton CA). Multi-burn solid fuel restartable rocket and method of use. USP1982114357795.
  17. Morris Joseph W. (Rancho Cordova CA) Carlson Russell W. (Folsom CA) Peterson Kevin L. (Sacramento CA) Reich Edward M. (Orangevale CA). Multiple pintle nozzle propulsion control system. USP1995105456425.
  18. Andrew James W. (Salt Lake City UT). Propellant grain design. USP1990064936092.
  19. Cesaroni,Anthony J.; Dennett,Michael J.; Louwers,Jeroen. Propellant system for solid fuel rocket. USP2006047022196.
  20. Krishnan, Vinu B.. Propulsion from combustion of solid propellant pellet-projectiles. USP2005116968676.
  21. Krishnan,Vinu B.. Propulsion from combustion of solid propellant pellet-projectiles. USP2007037194852.
  22. Alan Z. Glasser. Propulsion system. USP2002036357357.
  23. Hattori Nobuyoshi,JPX ; Yamana Kaoru,JPX ; Tamada Tomoki,JPX. Quality management system and recording medium. USP2001036202037.
  24. Canterberry J. B. (Taft TN) Flanigan David A. (Ogden UT). Rapid burning propellant charge for automobile air bag inflators, rocket motors, and igniters therefor. USP1991065024160.
  25. 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.
  26. Hibler Donald R. (Bates City MO) Hinrichs James O. (Odessa MO). Reverse bulged forward acting scored rupture disc bulkhead structure for multi-stage rocket motor. USP1992115160070.
  27. Whitesides ; Jr. Roger H. (Somerville AL). Rocket motor or gas generator having controlled thrust or mass flow output. USP1982084345427.
  28. Cavalleri, Robert J.; Olden, Thomas A.. Rocket motor with pellet and bulk solid propellants. USP2010037685940.
  29. Sowa, Armin. Rocket thrust chamber. USP2004036705076.
  30. Wilkinson, David B.; Cloyd, James S.. Solid fuel rocket thrust control. USP2011098015920.
  31. Woessner, George T.; Abel, Stephen G.; Peck, Ronald A.; Baker, Mark H.; Christensen, Donald J.. Solid propellant burn rate, propellant gas flow rate, and propellant gas pressure pulse generation control system and method. USP2011027886519.
  32. Dombrowski Daniel C. (Elkton MD) Frey Thomas J. (Elkton MD) Nevrincean Andrew G. (Elkton MD) Carr ; Jr. Clyde E. (Lincoln University PA). Solid propellant dual pulse rocket motor loaded case and ignition system and method of manufacture. USP1997025600946.
  33. Dombrowski Daniel C. (Elkton MD) Frey Thomas J. (Wilmington DE) Nevrincean Andrew G. (Oxford PA). Solid propellant dual pulse rocket motor loaded case and ignition system and method of manufacture. USP1997105675966.
  34. Carrier Joseph L. C. (Ste-Foy CAX) Constantinou Tryfon (Sillery CAX) Shea Charles J. (Ste-Foy CAX) Smith Donald L. (Ste-Foy CAX). Solid rocket motor with dual interrupted thrust. USP1990114972673.
  35. Goddard Charles W. (San Jose CA) Lucas John T. (Los Altos CA) Galvan Paul A. (San Jose CA). Solid-propellant-powered maneuvering system for spacecraft. USP1991115062593.
  36. Rohrbaugh,Eric M.; White,Jeffrey M.. Steerable, intermittently operable rocket propulsion system. USP2007107281367.
  37. Knight,Andrew F.. Super-staged and continuously staged rocket. USP2006027000377.
  38. Denoel Jean Denis,FRX ; Dumortier Andre,FRX. System for controlling a space vehicle by gating gas. USP1998065765367.
  39. Franz David Bruce (Ventura CA). Timed missile flight termination system. USP1977024007688.