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Method and apparatus for deploying a satellite network 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64G-001/10
출원번호 US-0529395 (1990-05-25)
발명자 / 주소
  • King Jan A. (Boulder) Beidleman Neal J. (Boulder CO)
출원인 / 주소
  • Orbital Sciences Corporation (Fairfax VA 02)
인용정보 피인용 횟수 : 68  인용 특허 : 0

초록

The effect of orbit plane precession is used to place a plurality of satellites into one or more desired orbit planes. The satellites are distributed within each desired orbit plane in a selected configuration. The satellites are transported into orbit on one or more frame structures referred to as

대표청구항

A method of deploying a network of a plurality of satellites in a plurality of orbit planes comprising the steps of: launching the plurality of satellites into an initial orbit having an initial orbit plane; transferring a first satellite from the initial orbit into a first orbit having a first orbi

이 특허를 인용한 특허 (68)

  1. Mueller, George E.; Cochran, David B.; Kohrs, Richard H., Active satellite dispenser for reusable launch vehicle.
  2. Scott, David D., Apparatus and methods for in-space satellite operations.
  3. Chamness Darrell S. ; Vincent Thomas Raymond, Cantilever, bi-level platform satellite dispenser.
  4. Furman,Michael J., Complimentary retrograde/prograde satellite constellation.
  5. Batla, Fawwad M.; Ho, Yiu-Hung M., Compound steering law for efficient low thrust transfer orbit trajectory.
  6. Chao, Chia-Chun; Kirkpatrick, Brian E.; Lin, Victor Shiaw-Jong; Janson, Siegfried W., Deployment and control algorithms for wheel cluster formations of satellites.
  7. Hall,Lars, Device and method for a spacecraft.
  8. Lively, Carey; Thorstenson, Eric, Dual spacecraft design and deployment system and method of use thereof.
  9. Batla, Fawwad M.; Ho, Yiu-hung M., Enhanced compound steering law for general low thrust mission.
  10. Chu, Peter Y., High capacity spacecraft.
  11. Joshi Abhay M., Lightweight miniaturized integrated microsatellite employing advanced semiconductor processing and packaging technology.
  12. Belbruno Edward A., Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  13. Belbruno Edward A., Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  14. Belbruno, Edward A., Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  15. Belbruno, Edward A., Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  16. Belbruno,Edward A., Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  17. Edward A. Belbruno, Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  18. Chethik Frank, Medium earth orbit communication satellite system.
  19. Koppel Christophe,FRX ; Valentian Dominique,FRX, Method and a system for launching satellites simultaneously on non-coplanar orbits by using highly eccentric orbits and.
  20. Beyer, Jean-Claude, Method for making a support base plate for an artificial satellite on a dispenser platform for a plurality of such satellites.
  21. David Anderman, Method of using dwell times in intermediate orbits to optimize orbital transfers and method and apparatus for satellite repair.
  22. Peterka, III, James J.; Caplin, Glenn N.; Aston, Richard W., Methods and apparatus for performing propulsion operations using electric propulsion systems.
  23. Croom Christopher Allen ; Snyder William Allen, Methods for accurately inserting satellite constellations into common orbit planes.
  24. Croom Christopher Allen ; Snyder William Allen, Methods for accurately inserting satellite constellations into common orbit planes.
  25. Aston, Richard W.; Tomzynska, Anna M.; Langmack, Michael J.; Peterka, III, James J., Modular core structure for dual-manifest spacecraft launch.
  26. Eller Howard S. ; Coronel Ramon ; Elliott Lee E. ; Barrett Alfred ; Lee David W. Y., Modular spacecraft architecture.
  27. Smolik John V. ; Ku Spencer C. ; Mactavish Andrew I. ; Spiwak Mark A., Modular spacecraft payload support structure.
  28. Rosen, Harold A., Molniya orbit satellite systems, apparatus, and methods.
  29. Williams Brian R. ; Cress Peter H., Multiple altitude satellite relay system and method.
  30. Aston, Richard W.; Tomzynska, Anna M.; Caplin, Glenn N., Multiple space vehicle launch system.
  31. Aston, Richard W.; Tomzynska, Anna M.; Caplin, Glenn N., Multiple space vehicle launch system.
  32. Bombled, Jean P.; Aubret, Jean P.; Laporte, Christophe, Multisatellite distributor for launcher.
  33. Das, Aniruddha; Vichnin, Herbert H.; Achee, Brenton B., On-orbit storage, plane change, and injection to final orbit of space vehicles.
  34. Benedict, Bryan, Piggyback satellite payload arrangement, a device for and method of attaching a piggyback satellite payload and adapter to be used for a piggyback satellite payload arrangement for launching the piggyback satellite.
  35. Smith, Philip; England, James; Darmody, Michael; Rubidoux, Jack, Platform and launch initiation system for secondary spacecraft for launch vehicle.
  36. Edward A. Belbruno, Procedure for generating operational ballistic capture transfer using a computer implemented process.
  37. Belbruno Edward A., Procedure for generating operational ballistic capture transfer using computer implemented process.
  38. Collyer Gordon L., Reducing satellite weight and cost.
  39. John E. Draim, Redundant satellite system.
  40. Michael B. DiVerde ; Kenneth N. Telford ; George J. Budris ; Christopher M. Gil ; John F. Steinmeyer, Satellite dispenser.
  41. Taormina, Frank; Chang, Donald C. D.; Yung, Kar W.; Cheng, David C.; Mayfield, William W.; Novak, III, John; Wang, Arthur W., Satellite system and method of deploying same.
  42. Sauzay, Emmanuel; Chabert, Nathanael, Satellite system comprising two satellites attached to each other and method for launching them into orbit.
  43. Caplin, Glenn N.; Rosen, Harold A.; Fowler, Harmon C., Satellites and satellite fleet implementation methods and apparatus.
  44. Caplin, Glenn N.; Rosen, Harold A.; Fowler, Harmon C., Satellites and satellite fleet implementation methods and apparatus.
  45. Graham, John A., Separation system with shock attenuation.
  46. Vichnin, Herbert H.; Goodzeit, Neil E.; Hentosh, David J., Side-by-side dual-launch arrangement with improved payload compatibility.
  47. Chu, Peter Y., Side-by-side multiple launch configuration.
  48. Poncet, Dominique; Prud Hon, Christophe; Guyot, Serge, Space vehicle comprising posts for forming a stack, stack comprising at least two such vehicles placed in a launcher, and method for releasing the vehicles.
  49. Budris George J. ; McGrath ; II Peter A. ; Toulouse Tony L. ; Catalano Richard J. ; Diverde Michael B., Spacecraft dispensing system.
  50. Field, Daniel W.; Askijian, Armen; Grossman, James; Smith, Alexander D., Stackable satellites and method of stacking same.
  51. Wang,Arthur W., System and method for continuous broadcast service from non-geostationary orbits.
  52. Lapins Uldis E. (Rancho Palos Verdes CA), System and method for deploying multiple probes.
  53. Kistler,Walter P.; Citron,Robert A.; Taylor,Thomas C., System and method for transportation and storage of cargo in space.
  54. Edward A. Belbruno, System and method of a ballistic capture transfer to L4, L5.
  55. 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.
  56. Fuller, John David, Systems and methods for satellite constellation launch using air-launched vehicles.
  57. Thomas Peter Emmons, Jr. ; Richard Scott Torkington ; James Edmund Klekotka, Technique for satellite constellation growth.
  58. Johnson Conor D. ; Wilke Paul S. ; Pendleton Scott C., Three-axis, six degree-of-freedom, whole-spacecraft passive vibration isolation system.
  59. Obry Daniel,FRX ; Pimont Raymond,FRX ; Chevalier Guy,FRX, Tilting adaptor for the carriage of several payloads on the same launcher.
  60. Benson, Greg; Fistonich, Matthew Anthony, Trusted decision support system and method.
  61. Benson, Greg; Fistonich, Matthew Anthony, Trusted decision support system and method.
  62. Benson,Greg; Fistonich,Matthew Anthony, Trusted decision support system and method.
  63. Benson, Greg; Fistonich, Matthew Anthony, Trusted monitoring system and method.
  64. Benson, Greg; Fistonich, Matthew Anthony, Trusted monitoring system and method.
  65. Benson, Greg; Fistonich, Matthew Anthony, Trusted monitoring system and method.
  66. Michael B. DiVerde ; Kenneth Norman Telford, Twin lobe spacecraft dispenser apparatus and method.
  67. Kronhaus, Igal, Unified orbit and attitude control for nanosatellites using pulsed ablative thrusters.
  68. Wilke Paul S. ; Johnson Conor D., Whole-spacecraft passive isolation devices.
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