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특허 상세정보

Thrusters

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-009/42   
미국특허분류(USC) 60/260 ; 244/169
출원번호 US-0037804 (1987-04-13)
우선권정보 GB-0009228 (1986-04-16)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 21  인용 특허 : 0
초록

A thruster for use in a spacecraft uses vaporized propellant in its combustion chamber (110). Normally two propellants are used of the kind used for main thrusters so that two vaporization chambers are needed. Pressure valves (108, 109) are controlled by electronic means (220) to maintain current pressure.

대표
청구항

An attitude and orbit control thruster for use in a spacecraft having liquid bipropellant thrusters, comprising: a combustion chamber having a thrust nozzle; a fuel tank for containing a supply of liquid fuel; an oxidizing agent tank for containing a supply of liquid oxidizing agent; a pair of vaporizing chambers, each having an inlet and an outlet; first conduit means connected between the fuel tank and the inlet of the one of the vaporizing chambers for conveying the fuel along a first path to said one vaporizing chamber for vaporization therein to for...

이 특허를 인용한 특허 피인용횟수: 21

  1. Carlson, Russell; Barr, Dustin; Yan, Allen. Attitude control system. USP2018039927217.
  2. Zonenberg, Andrew D.; Sanchez, Jason D.; Garbuz, Piotr A.. Distributed thrusters driven gas compressor. USP2016129528507.
  3. Sanchez, Jason D.; Garbuz, Piotr A.; Zonenberg, Andrew D.. Flight control using distributed micro-thrusters. USP2016059340280.
  4. Sarigul Klijn,Marti; Sarigul Klijn,Nesrin; Benson,Jim; Williams,Grant; Macklin,Frank. High propulsion mass fraction hybrid propellant system. USP2008077404288.
  5. Grainger,Chris; Macklin,Frank. Hybrid propulsion system. USP2006077069717.
  6. MacKlin,Frank; Grainger,Chris. Hybrid propulsion system. USP2009037503165.
  7. Macklin, Frank; Grainger, Chris. Hybrid propulsion system. USP2012018099945.
  8. Macklin, Frank. Hybrid rocket motor with annular, concentric solid fuel elements. USP2013098539753.
  9. McKinney,Bevin C.; Hudson,Gary C.. Integrated abort rocket and orbital propulsion system. USP2009027484692.
  10. Morris, Dennis E.; Little, Alfred. Launch abort and orbital maneuver system. USP2014058727283.
  11. Perdu Michel (Frejus FRX). Method and system for monitoring the propellant consumption of a space vehicle. USP1990124979119.
  12. Sanchez, Jason D.; Garbuz, Piotr A.; Zonenberg, Andrew D.. Nanomolecular solid state electrodynamic thruster. USP2017129845796.
  13. Sanchez, Jason D.; Garbuz, Piotr A.; Zonenberg, Andrew D.. Nanomolecular solid state electrodynamic thruster. USP2014088794930.
  14. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016019242745.
  15. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016109469419.
  16. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2017079696726.
  17. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016049302790.
  18. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016069365300.
  19. Gronland,Tor Arne; Westerberg,Bjorn; Bergman,Goran; Anflo,Kjell; Brandt,Jesper; Lyckfeldt,Ola; Agrell,Johan; Ersson,Anders; Jaras,Sven; Boutonnet,Magali; Wingborg,Niklas. Reactor for decomposition of ammonium dinitramide-based liquid monopropellants and process for the decomposition. USP2006117137244.
  20. Ellison John R.. Satellite control method using single species of bipropellant. USP2000026024328.
  21. Benson, Jim. Single-piece hybrid rocket motor. USP2011067966809.