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		<title>Orbital mechanics - Revision history</title>
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		<updated>2026-05-19T18:16:13Z</updated>
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		<id>http://wiki.newmars.com/index.php?title=Orbital_mechanics&amp;diff=399&amp;oldid=prev</id>
		<title>Josh Cryer: 1 revision</title>
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				<updated>2009-01-21T11:02:34Z</updated>
		
		<summary type="html">&lt;p&gt;1 revision&lt;/p&gt;
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				&lt;td colspan=&#039;1&#039; style=&quot;background-color: white; color:black; text-align: center;&quot;&gt;Revision as of 11:02, 21 January 2009&lt;/td&gt;
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		<author><name>Josh Cryer</name></author>	</entry>

	<entry>
		<id>http://wiki.newmars.com/index.php?title=Orbital_mechanics&amp;diff=398&amp;oldid=prev</id>
		<title>Josh Cryer: Reverted edit of OloviTaacm, changed back to last version by AdaptOrDie</title>
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				<updated>2009-01-20T13:24:47Z</updated>
		
		<summary type="html">&lt;p&gt;Reverted edit of OloviTaacm, changed back to last version by AdaptOrDie&lt;/p&gt;
&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;==Intro==&lt;br /&gt;
Most missions to mars are based on a [[Hohmann trajectory]]. This trajectory is the fastest trajectory possible that is minimum energy (based on the [[two body problem]]). Less energetic trajectories are available using the [[three body patched trajectories]] ([[Interplanetary super highway]]) but these can take a considerably longer length of time. &lt;br /&gt;
&lt;br /&gt;
For basic mission planning the [[delta V]] of the two body problem is used to calculate the [[mass fraction]] for the trip between [[Earth]] and [[Mars]]. The mass fraction tells mission planers how much mass they need to deliver to [[LEO]] in order to get a given mass to Mars. For calculating other trajectories Numeric or algebraic techniques can be used.&lt;br /&gt;
&lt;br /&gt;
Some useful algebraic techniques that will be presented shortly are:&lt;br /&gt;
&lt;br /&gt;
Finding the [[Orbital plane]] –Useful linear algebra for considering the three dimensional nature of the problem.&lt;br /&gt;
&lt;br /&gt;
[[Orbital Intersections]] –Useful geometry for finding where two orbits intersect each other.&lt;br /&gt;
&lt;br /&gt;
==Links to New Mars Discussions==&lt;br /&gt;
*[http://www.newmars.com/forums/viewtopic.php?t=2442 Orbital mechanics] First post: Mon Mar 15, 2004 12:04 pm, Last Post: Sun Jul 10, 2005 2:29 pm&amp;lt;br&amp;gt;&lt;br /&gt;
*[http://www.newmars.com/forums/viewtopic.php?t=2410 Zero energy trajectories - a thread to discuss this topic] First post, Thu Mar 25, 2004 5:47 pm, Last Post: Fri Apr 02, 2004 6:51 pm&lt;br /&gt;
&lt;br /&gt;
==Online Textbooks==&lt;br /&gt;
&lt;br /&gt;
*[http://ads.harvard.edu/books/1989fcm..book/ The Foundations of Celestial Mechanics]&lt;br /&gt;
&lt;br /&gt;
==External Links==&lt;br /&gt;
Orbital mechanics from: [[http://www.braeunig.us/space/orbmech.htm Rocket and Space technology]]&amp;lt;br&amp;gt;&amp;lt;br&amp;gt;&lt;br /&gt;
Orbital Mechanics form [[http://www.marsacademy.com/traj.htm The Mars academy]]&lt;br /&gt;
&lt;br /&gt;
[[Category:Interplanetary Transportation]]&lt;/div&gt;</summary>
		<author><name>Josh Cryer</name></author>	</entry>

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