Difference between revisions of "Orbital Dynamics"
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<math>F = \frac{Gm_{1}m_{2}}{r^{2}}</math> | <math>F = \frac{Gm_{1}m_{2}}{r^{2}}</math> | ||
| − | where G is the | + | where G is the [[Universal Gravitational Constant]] whose value is ''''insert value here'''', <math>m_1</math> is the mass of the first body, <math>m_2</math> is the mass of the second body, and r is the distance between them. |
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{{Cleanup}} | {{Cleanup}} | ||
| + | [[Category:Colonization]] | ||
| + | [[Category:Missions]] | ||
| + | [[Category:Mission Plans]] | ||
[[Category:Physics]] | [[Category:Physics]] | ||
| + | [[Category:Suborbital]] | ||
| + | [[Category:Transportation]] | ||
| + | [[Category:Spacecraft]] | ||
Revision as of 12:52, 18 February 2007
Orbital dynamics is the study of the motion of objects in the presence of gravitational forces of other bodies. All bodies provide a gravitational pull on other bodies surrounding it. The force exerted by two bodies on each other is given by
<math>F = \frac{Gm_{1}m_{2}}{r^{2}}</math>
where G is the Universal Gravitational Constant whose value is 'insert value here', <math>m_1</math> is the mass of the first body, <math>m_2</math> is the mass of the second body, and r is the distance between them.
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