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특허 상세정보

Spacecraft structure and method

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/22    B64G-001/50   
미국특허분류(USC) 244/158A ; 244/158R
출원번호 US-0193465 (1994-02-08)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 14  인용 특허 : 0
초록

Spacecraft structure for use in the construction of the outer wall of a spacecraft. The construction of the outer wall of the spacecraft includes a hollow cellular honeycomb material that is sandwiched between a thin outer curved solid panel and a thin solid inner panel that has at least a portion that has a substantially flat inner surface. The inner and/or outer panel have provisions for mounting at least a portion of the payload for the spacecraft utilizing a series of inserts secured to the inner or outer panel. The outer and/or inner spacecraft wall...

대표
청구항

A spacecraft structure having a curved outer surface, comprising: a generally cylindrical body structure comprising a series of panel members; at least one of said series of panel members comprising an inner panel, an outer panel, and a honeycomb member located between said inner panel and said outer panel, with said outer panel forming a portion of the curved outer surface of said spacecraft structure; and, at least one insert located in said inner panel for mounting payload to said spacecraft structure; said panel members providing sole load support fo...

이 특허를 인용한 특허 피인용횟수: 14

  1. Kutter, Bernard Friedrich; Zegler, Frank Charles; Willey, Cliff E.; Lin, John K.; Ragab, Mohamed M.; Dew, Michael W.. Cryogenic propellant depot and deployable sunshield. USP2012068196869.
  2. Kutter, Bernard Friedrich; Zegler, Frank Charles; Ragab, Mohamed R.. Cryogenic propellant depot and integral sunshield. USP2012068196868.
  3. Barrett Alfred. Externally mountable spacecraft equipment module. USP1999045897080.
  4. Eller Howard S. ; Coronel Ramon ; Giebler Martin M.. Functionally independent spacecraft module. USP1999085931418.
  5. Hand, Michael L.; Cook, Edward E.; Yao, Samuel S.. Integral node tubular spaceframe. USP2004096793183.
  6. Kolodziej Paul ; Bull Jeff ; Kowalski Thomas ; Switzer Matthew. Integrated thermal insulation system for spacecraft. USP1998095803406.
  7. Elliott Lee E. ; Barrett Alfred. Method for adjusting stiffness and acoustic properties of an externally mountable spacecraft equipment module. USP1999055904317.
  8. Fussell, Ronald M.; Ely, Donald W.; Meier, Gary M.; Halpin, Paul C.; Meade, Phillip T.; Jacobson, Craig A.; Blackwell-Thompson, Charlie. Methods and systems for advanced spaceport information management. USP2010127860684.
  9. Fussell,Ronald M.; Ely,Donald W.; Meier,Gary M.; Halpin,Paul C.; Meade,Phillip T.; Jacobson,Craig A.; Blackwell Thompson,Charlie. Methods and systems for advanced spaceport information management. USP2007117302364.
  10. Eller Howard S. ; Coronel Ramon. Modular spacecraft development process. USP1999105961076.
  11. Long, David S.. Multifunctional chambered radiation shields and systems and related methods. USP2014038678322.
  12. Cappa James O. ; Dursch Harry W.. One piece spacecraft frame. USP1998125848767.
  13. Maignan,Michel; Youssefi,Thierry; Brevart,Bertrand. Rigid multilayer material for thermal insulation. USP2006027001656.
  14. Hemingway Michael D. ; Hicks Glen W. ; Hull ; III Dwight E. ; Ritchie Michael D.. Thermal control system for spacecraft. USP2001056230790.