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Pulsed electrothermal thruster

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F03H-001/00   
미국특허분류(USC) 60/2031 ; 60/204
출원번호 US-0133154 (1987-12-07)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 22  인용 특허 : 1
초록
▼

A plasma electrothermal thruster includes a capillary passage in which a plasma discharge is formed and directed out of an open end of the passage into a supersonic nozzle. Liquid supplied to the capillary passage becomes partially atomized to cool a confining surface of the passage. The plasma discharge is formed as the atomized liquid flows out of the open end into a supersonic equilibrium nozzle. The discharge can have a duration greater than the two way travel time of acoustic energy in the capillary to cause the plasma to flow continuously through t...

대표
청구항
▼

An electrothermal thruster adapted to be mounted on a mass to be propelled comprising means for forming a capillary passage having an elongated plasma confining surface that is an outer boundary for plasma in the passage, the passage having an open end, electric means for forming a plasma discharge in the capillary passage, the capillary passage being arranged so that the plasma is ejected from the capillary passage only out of the open end, the ejected plasma being a thrust source for the mass, the plasma in the capillary passage having a very high pres...

이 특허에 인용된 특허 (1)

  1. Cann Gordon L. (P.O. Box 279 Laguna Beach CA 92652) ..UC: 60/2031 219/121PN 313/23141. Spacecraft optimized arc rocket. USP1986034577461.

이 특허를 인용한 특허 피인용횟수: 22

  1. William A. Hoskins ; Robert J. Cassady. ARC discharge initiation for a pulsed plasma thruster. USP2002046373023.
  2. Rooney,Kevin J.. Dual mode hybrid electric thruster. USP2008077395656.
  3. Roy,Subrata. Electric propulsion device for high power applications. USP2009037506497.
  4. Valentian, Dominique. Electrolytic igniter for rocket engines using liquid propellants. USP2013028375697.
  5. Valentian, Dominique. Electrolytic igniter for rocket engines using monopropellants. USP2013038387359.
  6. Mitchell, Stuart B.. Electrostatic transcutaneous hypodermic spray (electrostatic hypospray). USP2012038142391.
  7. Witherspoon F. Douglas ; Massey Dennis W. ; Kincaid Russell W.. High velocity pulsed wire-arc spray. USP1999126001426.
  8. Palmer, Miles R.. Launch vehicle and system and method for economically efficient launch thereof. USP2016109463881.
  9. Palmer, Miles R.. Launch vehicle and system and method for economically efficient launch thereof. USP2018019862506.
  10. Palmer, Miles R.. Launch vehicle and system and method for economically efficient launch thereof. USP20190210202209.
  11. Palmer, Miles R.; Brown, Jr., Glenn William. Launch vehicle and system and method for economically efficient launch thereof. USP2017049617016.
  12. Westmeyer,Paul A.; Mazaheri,Renee. Method and apparatus for moving a mass. USP2009037500477.
  13. Westmeyer,Paul A.; Mazaheri,Renee. Method and apparatus for moving a mass. USP2006037013988.
  14. Goldstein Yeshayahu Shyke A.. Method of generating a high pressure gas pulse using fuel and oxidizer that are relatively inert at ambient conditions. USP1999065909001.
  15. Byers David C. ; Lewis ; Jr. David H.. Micro pulsed plasma thruster and method of operating same. USP2001046216445.
  16. Kornfeld,G체nter; Schwertfeger,Werner; Lenz,Roland; Coustou,Gregory. Plasma-accelerator configuration. USP2006087084572.
  17. Witherspoon F. Douglas ; Massey Dennis W.. Pulsed electrothermal powder spray. USP2000096124563.
  18. Witherspoon F. Douglas ; Massey Dennis W.. Pulsed high energy synthesis of fine metal powders. USP1999085935461.
  19. Witherspoon F. Douglas ; Kincaid Russell W. ; Massey Dennis W.. Pulsed plasma jet paint removal. USP1999105970993.
  20. Land, III,H. Bruce; Simon,Daniel H.; Rice,Tharen. Pulsed plasma thruster and method of making. USP2007127302792.
  21. Spanjers Gregory G.. Pulsed plasma thruster with electric switch enabling use of a solid electrically conductive propellant. USP2000116153976.
  22. Cassady R. Joseph ; Myers Roger M. ; Osborne Robert D.. Three axis pulsed plasma thruster with angled cathode and anode strip lines. USP2001016173565.

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