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특허 상세정보

Propulsion system comprising plurality of individually selectable solid fuel motors

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-009/95    B64G-001/40    B64G-001/26    F02K-009/10    F02K-009/24    F02K-009/76   
출원번호 US-0844597 (2015-09-03)
등록번호 US-9790895 (2017-10-17)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Moreno IP Law LLC
인용정보 피인용 횟수 : 0  인용 특허 : 19
초록

A propulsion system for use with a satellite comprises a substrate, a communication network and a cluster of individually selectable solid fuel motors mounted on the substrate and operatively connected to the communication network. A controller is also operatively connected to the communication network and operative to select any one of more motors of the cluster of individually selectable solid fuel motors and transmit signals to fire the one or more motors of the individually selectable solid fuel motors. The substrate may have various configurations. ...

대표
청구항

1. A propulsion system for a satellite, comprising: a substrate;a communication network;a cluster of individually selectable solid fuel motors mounted on the substrate and A operatively connected to the communication network, each of the solid fuel motors comprising a metal housing encasing a solid propellant; anda controller operatively connected to the communication network and operative to select any one or more motors of the individually selectable solid fuel motors and transmit signals to fire the one or more motors of the individually selectable so...

이 특허에 인용된 특허 (19)

  1. Rastegar, Jahangir S.; Spinelli, Thomas. Actuators for gun-fired projectiles and mortars. USP2010097800031.
  2. Peter D. Lohn ; David H. Lewis ; Wingsiu R. Chan. Aerospike augmentation of microthruster impulse. USP2002126487844.
  3. Sawka, Wayne N.. Controllable digital solid state cluster thrusters for rocket propulsion and gas generation. USP2013068464640.
  4. Olden, Thomas A.; Wrigglesworth, Walter. Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof. USP2014098826640.
  5. Daniel W. Youngner. MEMS microthruster array. USP2002046378292.
  6. Nelson Steven D. ; Sipes William J. ; Hoffmaster David K.. Mems synthesized divert propulsion system. USP2001016178741.
  7. Adams, Christian; Gurley, Kenneth S.; Rohter, Tara Y.; Nelson, Patrick A.. Method and device for matrix of explosive cells. USP2012028119958.
  8. Nelson, Steven; Carvalho, Joe; Diamond, Michael N.. Methods and systems for defining addresses for pyrotechnic devices networked in an electronic ordnance system. USP2012078213151.
  9. Ketsdever Andrew D. ; Muntz Eric P.. Microthruster for heating a propellant, driving the vapors produced to a discharge section. USP2001076263665.
  10. Sanchez, Jason D.; Garbuz, Piotr A.; Zonenberg, Andrew D.. Nanomolecular solid state electrodynamic thruster. USP2014088794930.
  11. Nelson, Steven D.; Diamond, Michael N.. Networked electronic ordnance system. USP2010077752970.
  12. Nelson, Steven D.; Diamond, Michael N.. Networked electronic ordnance system. USP2012038136448.
  13. Nelson, Steven D.; Diamond, Michael N.; Walsh, John J.. Networked electronic ordnance system. USP2010017644661.
  14. Ritchie, Robert S.; Nelson, Steven D.; Diamond, Michael N.. Networked pyrotechnic actuator incorporating high-pressure bellows. USP2010077762189.
  15. Ritchie, Robert S.; Nelson, Steven David; Diamond, Michael N.. Networked pyrotechnic actuator incorporating high-pressure bellows. USP2011108037823.
  16. Joshi, Prakash B.; Gelb, Alan H.; Upschulte, Bernard L.; Green, B. David. Polyoxymethylene as structural support member and propellant. USP2005066904749.
  17. Hafner, Matthew T.; Balangue, Ruben; Clark, Danny D.; Westbrook, III, John William. Propellant compositions including stabilized red phosphorus, a method of forming same, and an ordnance element including the same. USP2014028641842.
  18. Knight,Andrew F.. Simple solid propellant rocket engine and super-staged rocket. USP2007087254936.
  19. Desai,Amish; Verma,Ravi Kant; Sivilotti,Massimo Antonio. Versatile cavity actuator and systems incorporating same. USP2006047021217.