Titik Lagrange (Malay Wikipedia)

Analysis of information sources in references of the Wikipedia article "Titik Lagrange" in Malay language version.

refsWebsite

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4wikipedia.org

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3web.archive.org

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2planetary.org

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2ulalaunch.com

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1iop.org

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1wolfram.com

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1caltech.edu

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1dartmouth.edu

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1bnf.fr

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1montana.edu

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1huffingtonpost.com

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1minorplanetcenter.org

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bnf.fr

gallica.bnf.fr

(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.

caltech.edu

cds.caltech.edu

Koon, W. S. (2006). Dynamical Systems, the Three-Body Problem, and Space Mission Design. m/s. 9. Unknown parameter |coauthors= ignored (|author= suggested) (bantuan) (16MB)

dartmouth.edu

math.dartmouth.edu

Leonhard Euler, De motu rectilineo trium corporum se mutuo attrahentium (1765)

discovery.com

news.discovery.com

"MISSION COMPLETE! WMAP FIRES ITS THRUSTERS FOR THE LAST TIME".

huffingtonpost.com

"Herschel Space Telescope Shut Down For Good, ESA Announces".

iop.org

iopscience.iop.org

ZF Seidov, "The Roche Problem: Some Analytics", The Astrophysical Journal, 603:283-284, 2004 March 1

minorplanetcenter.org

"List Of Neptune Trojans". Minor Planet Center. Diarkibkan daripada yang asal pada 2011-08-24. Dicapai pada 2010-10-27. Unknown parameter |deadurl= ignored (bantuan)

montana.edu

physics.montana.edu

Cornish, Neil J. "The Lagrangian Points" (PDF). Department of Physics, Bozeman Campus, Montana State University, USA. Diarkibkan daripada yang asal (PDF) pada 2015-09-07. Dicapai pada 29 July 2011.

nasa.gov

NASA—NASA's Wise Mission Finds First Trojan Asteroid Sharing Earth's Orbit

planetary.org

Lakdawalla, Emily (14 June 2012). "Chang'E 2 has departed Earth's neighborhood for.....asteroid Toutatis!?". Dicapai pada 15 Jun 2012.
"Update on yesterday's post about Chang'E 2 going to Toutatis". Planetary Society. 15 June 2012. Dicapai pada 26 June 2012.

space.com

Space.com: First Asteroid Companion of Earth Discovered at Last

springer.com

link.springer.com

Tantardini, Marco; Fantino, Elena (2010). "Spacecraft trajectories to the L₃ point of the Sun–Earth three-body problem". Celestial Mechanics and Dynamical Astronomy (Springer). Unknown parameter |coauthors= ignored (|author= suggested) (bantuan)

ulalaunch.com

Zegler, Frank (2010-09-02). "Evolving to a Depot-Based Space Transportation Architecture" (PDF). AIAA SPACE 2010 Conference & Exposition. AIAA. m/s. 4. Diarkibkan daripada yang asal (PDF) pada 2012-03-09. Dicapai pada 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. Unknown parameter |coauthors= ignored (|author= suggested) (bantuan)
Zegler, Frank; Bernard Kutter (2010-09-02). "Evolving to a Depot-Based Space Transportation Architecture" Diarkibkan 2012-03-09 di Wayback Machine. 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."

web.archive.org

Cornish, Neil J. "The Lagrangian Points" (PDF). Department of Physics, Bozeman Campus, Montana State University, USA. Diarkibkan daripada yang asal (PDF) pada 2015-09-07. Dicapai pada 29 July 2011.
Zegler, Frank (2010-09-02). "Evolving to a Depot-Based Space Transportation Architecture" (PDF). AIAA SPACE 2010 Conference & Exposition. AIAA. m/s. 4. Diarkibkan daripada yang asal (PDF) pada 2012-03-09. Dicapai pada 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. Unknown parameter |coauthors= ignored (|author= suggested) (bantuan)
Zegler, Frank; Bernard Kutter (2010-09-02). "Evolving to a Depot-Based Space Transportation Architecture" Diarkibkan 2012-03-09 di Wayback Machine. 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."

webcitation.org

"List Of Neptune Trojans". Minor Planet Center. Diarkibkan daripada yang asal pada 2011-08-24. Dicapai pada 2010-10-27. Unknown parameter |deadurl= ignored (bantuan)

wikipedia.org

en.wikipedia.org

Koon, W. S. (2006). Dynamical Systems, the Three-Body Problem, and Space Mission Design. m/s. 9. Unknown parameter |coauthors= ignored (|author= suggested) (bantuan) (16MB)
Zegler, Frank (2010-09-02). "Evolving to a Depot-Based Space Transportation Architecture" (PDF). AIAA SPACE 2010 Conference & Exposition. AIAA. m/s. 4. Diarkibkan daripada yang asal (PDF) pada 2012-03-09. Dicapai pada 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. Unknown parameter |coauthors= ignored (|author= suggested) (bantuan)
Tantardini, Marco; Fantino, Elena (2010). "Spacecraft trajectories to the L₃ point of the Sun–Earth three-body problem". Celestial Mechanics and Dynamical Astronomy (Springer). Unknown parameter |coauthors= ignored (|author= suggested) (bantuan)
"List Of Neptune Trojans". Minor Planet Center. Diarkibkan daripada yang asal pada 2011-08-24. Dicapai pada 2010-10-27. Unknown parameter |deadurl= ignored (bantuan)

wolfram.com

demonstrations.wolfram.com

"Lagrange Points" oleh Enrique Zeleny, Wolfram Demonstrations Project.