Rujukan Titik Lagrange

  1. ↑ ZF Seidov, "The Roche Problem: Some Analytics", The Astrophysical Journal, 603:283-284, 2004 March 1
  2. ↑ "Lagrange Points" oleh Enrique Zeleny, Wolfram Demonstrations Project.
  3. ↑ Koon, W. S. (2006). Dynamical Systems, the Three-Body Problem, and Space Mission Design. m/s. 9.  Parameter |coauthors= tidak diketahui diabaikan (guna |author=) (bantuan) (16MB)
  4. ↑ Leonhard Euler, De motu rectilineo trium corporum se mutuo attrahentium (1765)
  5. ↑ (Perancis) Lagrange, Joseph-Louis (1867–92). "Tome 6, Chapitre II: Essai sur le problème des trois corps". Oeuvres de Lagrange. Gauthier-Villars. m/s. 229–334. 
  6. ↑ Cornish, Neil J. "The Lagrangian Points" (PDF). Department of Physics, Bozeman Campus, Montana State University, USA. Dicapai 29 July 2011. 
  7. ↑ Farquhar, R. W.: "The Control and Use of Libration-Point Satellites", Ph.D. Dissertation, Dept. of Aeronautics and Astronautics, Stanford University, Stanford, CA, 1968
  8. ↑ Angular size of the Sun at 1 AU + 930000 miles: 31.6', angular size of Earth at 930000 miles: 29.3'
  9. ↑ "Herschel Space Telescope Shut Down For Good, ESA Announces". 
  10. ↑ Lakdawalla, Emily (14 June 2012). "Chang'E 2 has departed Earth's neighborhood for.....asteroid Toutatis!?". Dicapai 15 Jun 2012. 
  11. ↑ "Update on yesterday's post about Chang'E 2 going to Toutatis". Planetary Society. 15 June 2012. Dicapai 26 June 2012. 
  12. ↑ "MISSION COMPLETE! WMAP FIRES ITS THRUSTERS FOR THE LAST TIME". 
  13. ↑ Zegler, Frank (2010-09-02). "Evolving to a Depot-Based Space Transportation Architecture" (PDF). AIAA SPACE 2010 Conference & Exposition. AIAA. m/s. 4. Dicapai 2011-01-25. L2 is in deep space far away from any planetary surface and hence the thermal, micrometeoroid, and atomic oxygen environments are vastly superior to those in LEO. Thermodynamic stasis and extended hardware life are far easier to obtain without these punishing conditions seen in LEO. L2 is not just a great gateway- it is a great place to store propellants. ... L2 is an ideal location to store propellants and cargos: it is close, high energy, and cold. More importantly, it allows the continuous onward movement of propellants from LEO depots thus suppressing their size and effectively minimizing the near-earth boiloff penalties.  Parameter |coauthors= tidak diketahui diabaikan (guna |author=) (bantuan)
  14. ↑ Zegler, Frank; Bernard Kutter (2010-09-02). "Evolving to a Depot-Based Space Transportation Architecture". AIAA SPACE 2010 Conference & Exposition. AIAA. p. 4. Retrieved 2011-08-30. "We can create an energy savings account by moving propellant to the earth-moon Lagrange points—especially L2. Located 60,000 km beyond the Moon, propellant or cargo cached at L2 is very nearly at earth escape energy. It takes only a small nudge to dislodge it from Earth's gravitational grasp. This has been known for decades and L2 is often called a gateway to the solar system."
  15. ↑ Tantardini, Marco; Fantino, Elena (2010). "Spacecraft trajectories to the L3 point of the Sun–Earth three-body problem". Celestial Mechanics and Dynamical Astronomy (Springer).  Parameter |coauthors= tidak diketahui diabaikan (guna |author=) (bantuan)
  16. ↑ Space.com: First Asteroid Companion of Earth Discovered at Last
  17. ↑ NASA—NASA's Wise Mission Finds First Trojan Asteroid Sharing Earth's Orbit
  18. ↑ "List Of Neptune Trojans". Minor Planet Center. Diarkibkan daripada yang asal pada 2011-08-23. Dicapai 2010-10-27. 

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