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Method and a system for launching satellites on non-coplanar orbits, making the use of gravitational assistance from the moon

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64G-001/34
출원번호 US-0000896 (1997-12-30)
우선권정보 FR-0016275 (1996-12-31)
발명자 / 주소
  • Koppel Christophe,FRX
  • Valentian Dominique,FRX
출원인 / 주소
  • Societe Nationale d'Etude et de Construction de Moteurs d'Aviation, FRX
대리인 / 주소
    Weingarten, Schurgin, Gagnebin & Hayes LLP
인용정보 피인용 횟수 : 28  인용 특허 : 13

초록

A first satellite is placed practically directly by a launcher on a first final orbit. A second satellite is placed on the same launcher is initially transferred to a highly elliptical waiting orbit whose semi-major axis points to intercept the torus formed by the sphere of influence of the moon on

대표청구항

[ What is claimed is:] [1.] A method of launching satellites simultaneously on non-coplanar orbits, in which a first satellite is put on a launcher adapted to place said first satellite practically directly on a first final orbit having first orbital parameters with a first eccentricity value, a fir

이 특허에 인용된 특허 (13)

  1. Maute P. A. Alexandre (Valbonne FRX), Active three-axis attitude control system for a geostationary satellite.
  2. Gschel Wilhelm (Taufkirchen DEX), Method and apparatus for controlling a satellite.
  3. Frazier Scott R. (Herndon VA), Method for injecting payloads into orbit.
  4. Crill Philip D. (744 La Prenda Rd. Los Altos CA 94022) Kulick Shel (22364 Ramona Ct. Cupertino CA 95014), Method of placing a spacecraft into final earth orbit or earth escape trajectory.
  5. Uphoff Chauncey (Boulder CO), Orbital systems for cislunar travel.
  6. Achkar Issam-Maurice (Cannes la Bocca FRX) Renaud Pierre-Yves (Mandelieu FRX) Sghedoni Michel (Cannes FRX) Guillermin Pierre (Nice FRX), Rate gyro calibration method and apparatus for a three-axis stabilized satellite.
  7. Dulck Jean F. (Toulouse FRX), Satellite and method to place this satellite in orbit by gravitational assistance.
  8. Sackheim Robert L. (Palos Verdes CA) Hook Dale L. (Rancho Palos Verdes CA) Joseph Gary W. (Torrance CA), Satellite propulsion and power system.
  9. Perrotta Giorgio (Rome ITX), Satellite telecommunications and remote sensing system based on the use of short-period sun-synchronous elliptical orbit.
  10. Jones Ernest R. (Ormond Beach FL) Foley James P. (Yardley PA) Dockstader ; Jr. Robert K. (Morrisville PA), Spacecraft adapter and dispenser.
  11. Lichtin Daniel A. (Cranbury NJ) Raman Kidambi V. (East Windsor NJ) Subbarao Vasuki (Plainsboro NJ), Spacecraft velocity change maneuvers by variable arcjets.
  12. Hubert Susan M. (Cranbury NJ) Davies Keith (Robbinsville NJ), Spacecraft with increased stationkeeping fuel load.
  13. Smith Stanford S. (Boulder Creek CA) Marinos Gerasimos M. (Boulder Creek CA) Dimicelli Emanuel V. (Palo Alto CA), Technique for dispensing earth satellites into multi-planar orbits.

이 특허를 인용한 특허 (28)

  1. Healy, Liam M., Control system and method for a plane change for satellite operations.
  2. Jaeger, Talbot John; Ngo, Phong David, Delta-V-free satellite cloud cluster flying.
  3. Post, Kevin E.; Belbruno, Edward, Fast-low energy transfer to Earth-Moon Lagrange point L2.
  4. Everett, Matthew M.; Leuer, John P.; Whelan, David A.; Lambert, Stephen G., Laser communications following an atmospheric event.
  5. Belbruno Edward A., Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  6. Belbruno, Edward A., Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  7. Belbruno, Edward A., Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  8. Belbruno,Edward A., Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same.
  9. Sharer,Peter J., Method for deploying multiple spacecraft.
  10. Higgins, Robert P., Method for limiting interference between satellite communications systems.
  11. Higgins, Robert P., Method for limiting interference between satellite communications systems.
  12. Alfred Cellier, Overhead system of inclined eccentric geosynchronous orbiting satellites.
  13. Cellier Alfred, Overhead system of inclined eccentric geosynchronous orbitting satellites.
  14. Kistler,Walter P.; Citron,Robert A.; Taylor,Thomas C., Platform and system for mass storage and transfer in space.
  15. Kistler,Walter P; Citron,Robert A; Taylor,Thomas C, Platform and system for mass storage and transfer in space.
  16. Kistler,Walter P.; Citron,Robert A.; Taylor,Thomas C., Platform and system for propellant tank storage and transfer in space.
  17. Edward A. Belbruno, Procedure for generating operational ballistic capture transfer using a computer implemented process.
  18. Belbruno Edward A., Procedure for generating operational ballistic capture transfer using computer implemented process.
  19. Wang,Arthur W., Satellite communication system.
  20. Higgins, Robert P., Satellite communications system.
  21. Wang,Arthur W., Satellite communications system.
  22. 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.
  23. Wang,Arthur W., System and method for continuous broadcast service from non-geostationary orbits.
  24. Grover, Piyush; Andersson, Christian, System and method for controlling motion of spacecrafts.
  25. Grover, Piyush, System and method for estimating states of spacecraft in planet-moon environment.
  26. Healy, Liam M., System and method for maneuver plan for satellites flying in proximity using apocentral coordinate system.
  27. Kistler,Walter P.; Citron,Robert A.; Taylor,Thomas C., System and method for transportation and storage of cargo in space.
  28. Criado, Alfredo, Unmanned aerial vehicle.
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