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Spacecraft optimized arc rocket 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • F03H-001/00
출원번호 US-0506876 (1983-06-22)
발명자 / 주소
  • Cann Gordon L. (P.O. Box 279 Laguna Beach CA 92652) ..UC: 60/2031 219/121PN 313/23141
인용정보 피인용 횟수 : 33  인용 특허 : 1

초록

This invention relates to a thruster apparatus applicable to the environment of a space vehicle or satellite and operable for positioning such vehicle or satellite in the proper orbital location. The device utilizes a unique configuration of passageways to convey the propellant to a location adjacen

대표청구항

A thruster for use in an extraterrestrial vehicle comprising: (a) an outer casing; (b) a cathode mounted within said outer casing and having an end; (c) an anode mounted within said outer casing and spaced a predetermined distance from said cathode end, said predetermined distance defining a gap in

이 특허에 인용된 특허 (1)

  1. Krayenbuhl Harold A. (Fair Oaks CA) Dolgonas Gene (Carmichael CA) Rogers Charles J. (Placerville CA), Rocket nozzle system.

이 특허를 인용한 특허 (33)

  1. Dong, Chun Christine; McDermott, Wayne Thomas; Patrick, Richard E.; Schwarz, Alexander, Apparatus and method for removal of surface oxides via fluxless technique involving electron attachment and remote ion generation.
  2. Dong,Chun Christine; McDermott,Wayne Thomas; Patrick,Richard E.; Schwarz,Alexander, Apparatus and method for removal of surface oxides via fluxless technique involving electron attachment and remote ion generation.
  3. Dong, Chun Christine; McDermott, Wayne Thomas; Patrick, Richard E.; Schwarz, Alexander, Apparatus for removal of surface oxides via fluxless technique involving electron attachment and remote ion generation.
  4. Miller,Raanan A.; Nazarov,Erkinjon G.; Krylov,Evgeny; Eiceman,Gary A.; Kaufman,Lawrence A., Capacitive discharge plasma ion source.
  5. Smith William W. (Seattle WA) Knowles Steven C. (Seattle WA), Efficiency arcjet thruster with controlled arc startup and steady state attachment.
  6. Koch, Norbert, Electrostatic ion accelerator arrangement.
  7. Zurbach, Stéphan Joseph; Marchandise, Frédéric Raphaël Jean, Engine for a spacecraft, and spacecraft comprising such an engine.
  8. Leslie R. Warboys ; James A. Lukash ; Diana K. Mann, Hall effect electric propulsion system.
  9. Palmer, Miles R., Launch vehicle and system and method for economically efficient launch thereof.
  10. Palmer, Miles R., Launch vehicle and system and method for economically efficient launch thereof.
  11. Palmer, Miles R., Launch vehicle and system and method for economically efficient launch thereof.
  12. Palmer, Miles R.; Brown, Jr., Glenn William, Launch vehicle and system and method for economically efficient launch thereof.
  13. Krishnan, Mahadevan; Wilson, Kristi; Champagne, Kelan; Wright, Jason D.; Gerhan, Andrew N., Liquid metal ion thruster array.
  14. Jackson Bernard ; Sackheim Robert Lewis ; Rosenthal Richard Aaron, Low power arcjet propellant feed system.
  15. Hofer, Richard R., Magnetically-conformed, variable area discharge chamber for hall thruster, and method.
  16. Hilliard John C. (Ann Arbor MI), Method and apparatus for increasing radiant heat production of hydrocarbon fuel combustion systems.
  17. Miller,Raanan A.; Nazarov,Erkinjon G.; Krylov,Evgeny; Eiceman,Gary A.; Wright,John A.; Kendig,Stephen D.; Morris,C. James; Cameron,Douglas B., Method and apparatus for plasma generation.
  18. Miller,Raanan A.; Nazarov,Erkinjon G.; Krylov,Evgeny; Eiceman,Gary A.; Wright,John A.; Kendig,Stephen D.; Morris,C. James; Cameron,Douglas B., Method and apparatus for plasma generation.
  19. Bonnet, Jean-Paul; Lebedev, Anton; Moreau, Eric; Benard, Nicolas, Method and device for adjusting the mass flow rate of a gas stream.
  20. Tillotson, Brian J., Methods and systems for flux distribution within a heat exchanger.
  21. Keidar, Michael; Shashurin, Alexey; Zhuang, Tai Sen, Micro-cathode thruster and a method of increasing thrust output for a micro-cathode thruster.
  22. Keidar, Michael; Shashurin, Alexey; Zhuang, Taisen, Micro-cathode thruster and a method of increasing thrust output for a micro-cathode thruster.
  23. Manzoni, Giulio, Micro-nozzle thruster.
  24. Knowles Steven C. (Seattle WA), Non-erosive arcjet starting control system and method.
  25. Marhic Grard (Cergy FRX) Messager Jol (Bessancourt FRX), Plasma arc forming process and device.
  26. Hatch Bruce O. (Lebanon NH), Plasma arc gouger.
  27. Burton Rodney L. (Fairfax Station VA) Goldstein Yeshayahu S. A. (Gaithersburg MD) Tidman Derek A. (Silver Spring MD) Winsor Niels K. (Alexandria VA), Pulsed electrothermal thruster.
  28. Burton Rodney L. (Fairfax Station VA) Goldstein Yeshayahu S. A. (Gaithersburg MD) Tidman Derek A. (Silver Spring MD) Winsor Niels K. (Alexandria VA), Pulsed electrothermal thruster.
  29. Spanjers Gregory G., Pulsed plasma thruster with electric switch enabling use of a solid electrically conductive propellant.
  30. Calabro, Max, Resistojet.
  31. Valdes, Marcelo Esteban; Asokan, Thangavelu, System and apparatus for arc elimination.
  32. Nagao, Toru; Morita, Naoki, Thruster and spacecraft.
  33. Steenborg, Manfred, Thruster for spacecraft.
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