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특허 상세정보

Modular divert and attitude control system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/00    F42B-015/01    F42B-015/00   
미국특허분류(USC) 244/003.1; 060/200.1; 060/204; 060/224; 060/225; 060/253; 102/283; 244/003.15; 244/003.21; 244/003.22
출원번호 US-0484986 (2009-06-15)
등록번호 US-8242422 (2012-08-14)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Gifford, Eric A.
인용정보 피인용 횟수 : 6  인용 특허 : 28
초록

There is disclosed a vehicle and methods for maneuvering the vehicle. The vehicle may include a plurality of multiple-impulse rocket motors, each of which comprises a plurality of independently ignitable solid fuel propellant charges, and a processor that generates at least one command to ignite at least one solid fuel propellant charge of at least one of the plurality of multiple-impulse rocket motors.

대표
청구항

1. A vehicle, comprising: a plurality of multiple-impulse rocket motors, each of which comprises a plurality of independently ignitable solid fuel propellant charges; anda processor that generates at least one command to ignite at least one solid fuel propellant charge of at least one of the plurality of multiple-impulse rocket motors. 2. The vehicle of claim 1, wherein each multiple-impulse rocket motor further comprises: a nozzle, anda plurality of combustion chambers coupled to the nozzle, whereineach of the plurality of combustion chambers at least p...

이 특허에 인용된 특허 (28)

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  2. 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.
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  8. Woessner, George T.. Missile thrust system and valve with refractory piston cylinder. USP2005056895991.
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  10. Bastian Thomas W. (Fullerton CA) Roberts J. Sydney (Fullerton CA). Multi-burn solid fuel restartable rocket and method of use. USP1982114357795.
  11. 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.
  12. Cesaroni,Anthony J.; Dennett,Michael J.; Louwers,Jeroen. Propellant system for solid fuel rocket. USP2006047022196.
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  16. 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.
  17. Whitesides ; Jr. Roger H. (Somerville AL). Rocket motor or gas generator having controlled thrust or mass flow output. USP1982084345427.
  18. Cavalleri, Robert J.; Olden, Thomas A.. Rocket motor with pellet and bulk solid propellants. USP2010037685940.
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  20. Wilkinson, David B.; Cloyd, James S.. Solid fuel rocket thrust control. USP2011098015920.
  21. 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.
  22. 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.
  23. 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.
  24. 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.
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