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Satellites and satellite fleet implementation methods and apparatus

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64G-001/10
출원번호 US-0693645 (2007-03-29)
등록번호 US8016240 (2011-08-30)
발명자 / 주소
  • Caplin, Glenn N.
  • Rosen, Harold A.
  • Fowler, Harmon C.
출원인 / 주소
  • The Boeing Company
대리인 / 주소
    Yee & Associates, P.C.
인용정보 피인용 횟수 : 9  인용 특허 : 46

초록

A method for implementing a satellite fleet includes launching a group of satellites within a launch vehicle. In an embodiment, the satellites are structurally connected together through satellite outer load paths. After separation from the launch vehicle, nodal separation between the satellites is

대표청구항

What is claimed is: 1. A method for implementing a satellite fleet, wherein the satellite fleet includes multiple-satellites whose orbital planes have separated nodes, the method comprising:launching a first launch vehicle, which contains a first group of the multiple satellites within a first paylo

이 특허에 인용된 특허 (46)

  1. Turner Andrew E. (Palo Alto CA), Apogee at constant time-of-day equatorial (ACE) orbit.
  2. Mass Jonathan,ILX, Artificial satellite communication system.
  3. Agrawal Brij N. (9 Thorburn Pl. Gaithersburg MD 20878) Madon Pierre J. (1033 - 22nd St. ; N.W. Washington DC 20037), Attitude pointing error correction system and method for geosynchronous satellites.
  4. Maeda, Toshihide; Hamano, Nobuo; Nakamura, Shigeki; Yoshida, Tomiharu; Owada, Masataka; Ikeda, Masahiko; Yabutani, Takashi; Ito, Masahiro, Communication system, communication receiving device and communication terminal in the system.
  5. John E. Draim, Constellation of elliptical orbit satellites with line of apsides lying in or near the equatorial plane.
  6. Goodzeit, Neil Evan, Constellation of spacecraft, and broadcasting method using said constellation.
  7. Cellier Alfred ; Rey Raul D., Coordinatable system of inclined geosynchronous satellite orbits.
  8. Cellier Alfred ; Rey Raul D., Coordinatable system of inclined geosynchronous satellite orbits.
  9. Kellberg,Christian J., Deployable spacecraft mount for electric propulsion.
  10. Briskman Robert D. ; Nelson Robert A., Efficient high latitude service area satellite mobile broadcasting systems.
  11. Briskman, Robert D.; Nelson, Robert A., Efficient high latitude service area satellite mobile broadcasting systems.
  12. Castiel David (Washington DC) Draim John E. (Washington DC) Brosius Jay (Washington DC), Elliptical orbit satellite, system, and deployment with controllable coverage characteristics.
  13. Castiel David (Washington DC) Draim John E. (Washington DC) Brosius Jay (Washington DC), Elliptical orbit satellite, system, and deployment with controllable coverage characteristics.
  14. Castiel David ; Draim John ; Brosius Jay ; Schor Matthew, Elliptical orbit satellite, system, and deployment with controllable coverage characteristics.
  15. Castiel David ; Draim John ; Brosius Jay ; Schor Matthew, Elliptical orbit satellite, system, and deployment with controllable coverage characteristics.
  16. Salvatore Jeremiah O. ; Ocampo Cesar A., Free return lunar flyby transfer method for geosynchronous satellites.
  17. Stuart James R. ; Sturza Mark Alan ; Patterson David P., Frequency sharing for satellite communication system.
  18. Kartalopoulos Stamatios V. (Annandale NJ), Global multi-satellite network.
  19. Wiedeman Robert A, Interactive fixed and mobile satellite network.
  20. Wiedeman Robert A., Interactive fixed and mobile satellite network.
  21. King Jan A. (Boulder) Beidleman Neal J. (Boulder CO), Method and apparatus for deploying a satellite network.
  22. Anzel Bernard M., Method and apparatus for stationkeeping a satellite offset by pitch rotation.
  23. Frazier Scott R. (Herndon VA), Method for injecting payloads into orbit.
  24. Higgins, Robert P., Method for limiting interference between satellite communications systems.
  25. Higgins, Robert P., Method for limiting interference between satellite communications systems.
  26. Anzel Bernard M. (Venice CA), Method for satellite station keeping.
  27. Vorlicek Preston L. (Memphis TN), Method for spinning up a three-axis controlled spacecraft.
  28. Yocum ; Jr. John F. ; Cazeau Patrick A. ; Koffman Stephen J. ; Baker Douglas A., Method of controlling attitude of a momentum biased spacecraft during long-duration thruster firings.
  29. Hosick Daryl K. ; Gelon Walter S. ; Mills Richard M., Multiple usage thruster mounting configuration.
  30. Castiel David, Non-geostationary orbit satelite constellation for continuous preferential coverage of northern latitudes.
  31. Castiel, David, Non-geostationary orbit satellite constellation for continuous coverage of northern latitudes.
  32. Castiel David, Non-geostationary orbit satellite constellation for continuous coverage of northern latitudes above 25.degree. and its e.
  33. Alfred Cellier, Overhead system of inclined eccentric geosynchronous orbiting satellites.
  34. Cellier Alfred, Overhead system of inclined eccentric geosynchronous orbitting satellites.
  35. Anzel Bernard M., Satellite co-location methods.
  36. Higgins, Robert P., Satellite communications system.
  37. Torkington Richard S. ; Emmons ; Jr. Thomas P. ; Warble Keith, Satellite communications systems using satellites in a zero-drift constellation.
  38. Ellison John R., Satellite control method using single species of bipropellant.
  39. Perrotta Giorgio (Rome ITX), Satellite telecommunications and remote sensing system based on the use of short-period sun-synchronous elliptical orbit.
  40. Budris George J. ; McGrath ; II Peter A. ; Toulouse Tony L. ; Catalano Richard J. ; Diverde Michael B., Spacecraft dispensing system.
  41. Harwood Oliver P. (Huntington Beach CA) Love John A. (Seal Beach CA), Spacecraft for use in conjunction with a reusable space shuttle.
  42. Draim, John E., System and method for implementing a constellation of non-geostationary satellites that does not interfere with the geostationary satellite ring.
  43. Draim, John E., System and method for implementing a constellation of non-geostationary satellites that provides simplified satellite tracking.
  44. Goodzeit, Neil Evan; Ratan, Santosh, System for high efficiency spacecraft orbit transfer.
  45. Draim John E. (9310 Telfer Ct. Vienna VA 22180), Tetrahedral multi-satellite continuous-coverage constellation.
  46. Ratan Santosh (Lawrenceville NJ) Goodzeit Neil Evan (Princeton NJ), Universal thruster selection logic for spacecraft attitude control.

이 특허를 인용한 특허 (9)

  1. Chao, Chia-Chun; Kirkpatrick, Brian E.; Lin, Victor Shiaw-Jong; Janson, Siegfried W., Deployment and control algorithms for wheel cluster formations of satellites.
  2. Peterka, III, James J.; Caplin, Glenn N.; Aston, Richard W., Methods and apparatus for performing propulsion operations using electric propulsion systems.
  3. Aston, Richard W.; Tomzynska, Anna M.; Langmack, Michael J.; Peterka, III, James J., Modular core structure for dual-manifest spacecraft launch.
  4. Aston, Richard W.; Tomzynska, Anna M.; Caplin, Glenn N., Multiple space vehicle launch system.
  5. Aston, Richard W.; Tomzynska, Anna M.; Caplin, Glenn N., Multiple space vehicle launch system.
  6. Aston, Richard W.; Tomzynska, Anna M.; Caplin, Glenn N., Multiple space vehicle launch system.
  7. Caplin, Glenn N.; Rosen, Harold A.; Fowler, Harmon C., Satellites and satellite fleet implementation methods and apparatus.
  8. Higham, John; Tilley, Scott, Spacecraft transfer orbit techniques.
  9. Balemboy, Christophe; Laine, Robert Andre; Sembely, Xavier, System comprising a spatial mother probe forming a spatial carrier vehicle and a plurality of spatial daughter probes.
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