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특허 상세정보

Active spacecraft thermal control system and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/58   
미국특허분류(USC) 244/163 ; 165/041
출원번호 US-0842106 (1997-04-28)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Whitney
인용정보 피인용 횟수 : 15  인용 특허 : 7
초록

A spacecraft (10) has combined propulsion and active thermal control systems. A propellant storage tank (20) couples to a pressurant storage tank (18). A working fluid (52) resides in the pressurant storage tank (18) and propels propellant when needed while concurrently acting as a thermal working fluid. The working fluid (52) is expanded then routed to selected cooled components (64). After passing by the cooled components (64), the working fluid (52) is compressed and passed by selected heated components (82). A controller (36) monitors temperature sen...

대표
청구항

[ What is claimed is:] [1.] A spacecraft having a combined propulsion and active thermal control system, said spacecraft comprising:a first component which includes a propellant valve;a second component which includes a battery, wherein said second component is active and temperature sensitive;a storage tank which contains a propulsion system fluid;a pump;a thruster;a power amplifier; anda conduit system coupled to said tank, said pump, said first component, said second component, said thruster, and said power amplifier, said conduit system including sai...

이 특허를 인용한 특허 피인용횟수: 15

  1. Robert T. Bigelow ; Russell J. Common ; John Mezits ; David A. Cavaleri. Apparatus for spacecraft thermal management. USP2002116481670.
  2. Walker, Andrew. Artificial Satellite. USP20181110118717.
  3. Combes,Charles; Foucher,Jean Luc; Jaubert,Pierre. Dual conduction heat dissipating system for a spacecraft. USP2006057048233.
  4. Cluzet, Gerard; Amidieu, Marcel; Tjiptahardja, Tisna. Heat transfer device. USP2003096626231.
  5. Braitmaier,Klaus; Multhaupt,Hans Dieter; Schmidt,Bernd. Method and device for adjusting a vehicle reclining seat. USP2007107281760.
  6. Schwarting Walter,DEX. Method and liquid storage tank for minimizing permeation of liquid vapors through a tank dividing membrane. USP2001056231008.
  7. Jaeger, Talbot. Method of cooling satlet electronics. USP2016069376222.
  8. Calabro, Max. Resistojet. USP2010067743601.
  9. Gelon Walter S. ; Hall John C. ; Goodman Christian J.. Sequenced heat rejection for body stabilized geosynchronous satellites. USP2000066073888.
  10. Mena, Fabrice. Spacecraft. USP20181210144534.
  11. Mena, Fabrice; Coutal, Patrick. Spacecraft. USP2017119828116.
  12. Eddy M. Yee. Spacecraft multiple loop heat pipe thermal system for internal equipment panel applications. USP2002116478258.
  13. Low, Lenny; Sebata, Susan. Spacecraft radiator system and method using cross-coupled deployable thermal radiators. USP2005026854510.
  14. Barton,Mark Carl; Miller,Jonathon. Thermal design for spacecraft modules. USP2007037191984.
  15. Cho, Wei-Lin; Adamson, Gary A.. Variable heat rejection using heat pipe heat exchanger. USP2018049939203.