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Spacecraft sunshield for use in performing solar torque balancing

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64G-001/24
출원번호 US-0638841 (2000-08-14)
발명자 / 주소
  • Mark A. Blair
출원인 / 주소
  • Ball Aerospace & Technologies Corp.
대리인 / 주소
    Sheridan Ross P.C.
인용정보 피인용 횟수 : 8  인용 특허 : 30

초록

A spacecraft includes an articulating sunshield assembly that is capable of simultaneously performing thermal control functions and solar torque balancing for the spacecraft. The sunshield assembly includes a pair of shield members that can be controllably positioned as the spacecraft orbits about a

대표청구항

1. A method for deploying at least a first shield member connected to a spacecraft body, comprising:providing a spacecraft that includes a spacecraft body and at least a first shield member connected to said spacecraft body; and deploying said first shield member relative to said spacecraft body in

이 특허에 인용된 특허 (30)

  1. Basuthakur Sibnath ; Bonello David Paul ; Allen Robert David, Actively controlled thermal panel and method therefor.
  2. Flament Patrick (Le Cannet FRX) Perdu Michel (Frejus FRX) Portier Jean (Cannes FRX) Brunet Pierre (Auribeau S/Siagne FRX), Apparatus controlling the pitch attitude of a satellite by means of solar radiation pressure.
  3. Kaufman David A., Apparatus for spacecraft angular momentum control through the use of reflective thermal blankets.
  4. Guenther Hans-Jrgen (Bremen DEX) Nauck Joachim (Bremen DEX) Renner Udo (Leiden DEX) Fehse Wigbert (Lisse DEX), Attitude control for satellites.
  5. Goodzeit Neil Evan (Princeton NJ) Ratan Santosh (Lawrenceville NJ), Attitude control for spacecraft with movable appendages such as solar panels.
  6. Damilano Patrice,FRX, Control of the attitude of a satellite in low orbit involving solar acquisition.
  7. Castiel David (Washington DC) Draim John E. (Washington DC) Brosius Jay (Washington DC), Elliptical orbit satellite, system, and deployment with controllable coverage characteristics.
  8. Eller Howard S. ; Coronel Ramon ; Giebler Martin M., Functionally independent spacecraft module.
  9. Stuart James R. (Louisville CO) Patterson David Palmer (Los Altos CA), Inflatable torus and collapsible hinged disc spacecraft designs for satellite communication system.
  10. Salvatore Jeremiah O. (Redondo Beach CA) Wittmann Alois (Palos Verdes CA), Method and apparatus for satellite torque balancing.
  11. Flament Patrick (Le Cannet FRX) Perdu Michel (Frejus FRX) Portier Jean (Cannes FRX) Brunet Pierre (Auribeau S/Siagne FRX), Method for controlling the pitch attitude of a satellite by means of solar radiation pressure and satellite, in particul.
  12. Surauer Michael (Chieming DEX) Bittner Helmut (Munich DEX), Method of adjusting the position of satellites by means of solar pressure torques.
  13. Bouzat Charles (Ramonville FRX), Method of placing a geostationary telecommunicaiton satellite in orbit.
  14. Perkins Frederick W. (McLean VA) Kananen Phil (Suitland MD), Modular mother satellite bus for subsidiary payloads.
  15. Faget Maxime A. (Dickinson TX) Johnson Caldwell C. (Dickinson TX) Bergeron ; III David J. (Houston TX), Modular spacecraft system.
  16. Polites Michael E. (Huntsville AL), Rotating-unbalanced-mass devices and methods for scanning balloon-borne-experiments, free-flying spacecraft, and space s.
  17. Rosen Harold A. (Santa Monica CA), Satellite control system.
  18. Tadros Alfred H. (Palo Alto CA), Satellite gravity gradient compensation using on-orbit solar array reorientation.
  19. Sullivan John M., Satellite solar array and method of biasing to reduce seasonal output power fluctuations.
  20. Lehner John A. (Sunnyvale CA) Holmes Thomas (Portola Valley CA), Satellite stabilization system.
  21. Shiki Haruo (Tokyo JPX), Shading device for use in a geostatic satellite.
  22. Harvey Thomas J. (Los Altos Hills CA) Gibson Gary C. (Los Gatos CA), Space satellite with agile payload orientation system.
  23. Decanini Jorge H. (Long Beach CA), Spacecraft control by electrochromic devices.
  24. Fuldner William V. (Lower Makefield Township ; Morrisville County PA) Ganssle Eugene R. (Skillman NJ), Spacecraft structure with symmetrical mass center and asymmetrical deployable appendages.
  25. Zimbelman Darrell F. (Gaithersburg MD), Spacecraft thermal disturbance control system.
  26. Foley James Paul ; Murray Bronson, Spacecraft with active antenna array protected against temperature extremes.
  27. Johnson Caldwell C. (Dickinson TX) Faget Maxime A. (Dickinson TX) Bergeron ; III David J. (Friendswood TX), Spacecraft with articulated solar array.
  28. Merhav Tamir R. (Freehold NJ) Festa Michael T. (Yardley PA) Stetson ; Jr. John B. (New Hope PA), Spacecraft with gradual acceleration of solar panels.
  29. Clark John F. (Princeton NJ), Station-keeping using solar sailing.
  30. Barker Lee A. ; Lange Benjamin, Using reflected solar radiation pressure to provide stationkeeping maneuvering of a spacecraft.

이 특허를 인용한 특허 (8)

  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.
  2. Kutter, Bernard Friedrich; Zegler, Frank Charles; Ragab, Mohamed R., Cryogenic propellant depot and integral sunshield.
  3. Dailey,Dean R.; Lillie,Charles F.; Flannery,Martin; Arenberg,Jonathan W.; Bronowicki,Allen J., Isolating positioning boom for instrument platform.
  4. Polle, Bernard, Method of controlling the attitude of a satellite and an attitude-controlled satellite.
  5. Leyre, Xavier, Satellite provided with means for countering solar pressure.
  6. Wehner, James; Rudd, Lael; Harris, Christian; Foroozan, Shahram, Solar array momentum control.
  7. Segal, Matthew Jonathan; Wise, Kevin Andrew, Solar energy collection flight path management system for aircraft.
  8. Dailey, Dean R.; Dailey, Nicholas B., Starshade with attributes facilitating assembly.
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