$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Apparatus for spacecraft thermal management

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/46   
미국특허분류(USC) 244/163; 244/1580R; 165/041
출원번호 US-0693534 (2000-10-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Sierra Patent Group, Ltd.
인용정보 피인용 횟수 : 12  인용 특허 : 5
초록

The present invention provides a thermal, and if desired, a radiation barrier to protect the exterior surface of a spacecraft. In particular, the present invention protects the polymeric materials of construction utilized in inflatable and expandable spacecraft from the deleterious effects of both thermal and radiation aging. The protective barrier is formed from a tube or tubes through which a fluid circulates. The tube segment substantially enclose the spacecraft, and in particular, the critical layers that are desired to be protected. This protective ...

대표
청구항

1. Apparatus for spacecraft thermal management comprising:a. a thermal radiator to reject heat; b. a pump, said pump having a first port and a second port, the first port of said pump connected to said thermal radiator; c. a tube, said tube substantially covering a surface of the spacecraft, one end of said tube connected to the second port of said pump, the other end of said tube connected to said thermal radiator, said tube, said thermal radiator, and said pump in fluid communication to form a continuous fluid flow loop, and d. a fluid, said pump circu...

이 특허를 인용한 특허 피인용횟수: 12

  1. Kinstler, Gary A.. Cryogenically cooled radiation shield device and associated method. USP2015079090360.
  2. Kinstler, Gary A.. Cryogenically cooled radiation shield device and associated method. USP2014088809824.
  3. Jacqu?,Bernard; Texier,Emmanuel; Cluzet,G?rard; Tjiptahardja,Tisna; Amidieu,Marcel. Heat transfer system for a satellite including an evaporator. USP2007027174950.
  4. Gayrard,Jean Didier; Belis,Eric; Michard,Fr챕d챕ric. Modular architecture for thermal control in a spacecraft. USP2006117131484.
  5. Mills, Gary L.; Unruh, Bryce W.; Rohrschneider, Reuben R.. Multi-layer insulation. USP2018049944452.
  6. Long, David S.. Multifunctional chambered radiation shields and systems and related methods. USP2014038678322.
  7. Kistler,Walter P.; Citron,Robert A.; Taylor,Thomas C.. Platform and system for mass storage and transfer in space. USP2006107118077.
  8. Kistler,Walter P; Citron,Robert A; Taylor,Thomas C. Platform and system for mass storage and transfer in space. USP2008057370835.
  9. Kistler,Walter P.; Citron,Robert A.; Taylor,Thomas C.. Platform and system for propellant tank storage and transfer in space. USP2007017156348.
  10. Bigelow, Robert T.. Radiation shield. USP2010087780118.
  11. Taylor,Thomas C.; Kistler,Walter P.; Citron,Robert A.. Space transportation node including tether system. USP2009037503526.
  12. Kistler,Walter P.; Citron,Robert A.; Taylor,Thomas C.. System and method for transportation and storage of cargo in space. USP2006107114682.