123 lines
5.8 KiB
HTML
123 lines
5.8 KiB
HTML
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<title>OpenRocket — Documentation</title>
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You are using a browser that is <strong>8 years old!</strong>
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In Internet-years that is <em>prehistoric!</em><br/>
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<em>please <a href="http://www.mozilla.com/">upgrade</a></em>. It's easy!
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<a href="http://sourceforge.net/projects/openrocket"><img src="http://sflogo.sourceforge.net/sflogo.php?group_id=260357&type=12" width="120" height="30" alt="Get OpenRocket at SourceForge.net. Fast, secure and Free Open Source software downloads" /></a>
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<h1>Documentation for OpenRocket</h1>
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<div class="content">
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<h2>User documentation</h2>
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<p>Unfortunately no user's guide currently exists for OpenRocket.
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Some documentation is available in the
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<a href="http://wiki.openrocket.info/">OpenRocket
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wiki pages</a>, including a stub
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<a href="http://wiki.openrocket.info/User%27s_Guide">User's
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guide</a> and a section of
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<a href="http://wiki.openrocket.info/FAQ">frequently
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asked questions</a>.</p>
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<p>If you would like to help, please extend the documentation!</p>
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<h2>Technical documentation</h2>
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<p>OpenRocket was originally written as the Master's thesis of
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Sampo Niskanen at Helsinki University of Technology. This thesis
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is being extended and updated as the OpenRocket technical
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documentation. Below is the latest technical documentation and
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the original Master's thesis.</p>
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<div class="separated">
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<p>
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<span class="licenseimage"><a rel="license" href="http://creativecommons.org/licenses/by-sa/3.0/"><img alt="CC BY-SA" src="cc-by-sa-80x15.png" /></a></span>
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<a href="techdoc.pdf">OpenRocket technical documentation</a> (2013-05-10)
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<span class="note">(PDF 1.4MB)</span>
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</p>
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<p>
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<span class="licenseimage"><a rel="license" href="http://creativecommons.org/licenses/by-nc-nd/3.0/"><img alt="CC BY-NC-ND" src="cc-by-nc-nd-80x15.png" /></a></span>
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<a href="thesis.pdf">Development of an Open Source model rocket simulation software</a> (Master's thesis)
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<span class="note">(PDF 1.3MB)</span>
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</p>
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</div>
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<p>The technical documentation is licensed under a
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<a rel="license" href="http://creativecommons.org/licenses/by-sa/3.0/">Creative Commons Attribution-ShareAlike License</a>
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while the Master's thesis is licensed under a
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<a rel="license" href="http://creativecommons.org/licenses/by-nd-nc/1.0/fi/deed.en">Attribution-NonCommercial-NoDerivs
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License</a>.
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</p>
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<p class="quote"><strong>Table of contents:</strong></p>
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<ol class="toc">
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<li>1. Introduction</li>
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<li>2. Basics of model rocket flight</li>
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<li>3. Aerodynamic properties of model rockets</li>
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<li>4. Flight simulation</li>
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<li>5. The OpenRocket simulation software</li>
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<li>6. Comparison with experimental data</li>
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<li>7. Conclusion</li>
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</ol>
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<ol class="toc">
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<li>A. Nose cone and transition geometries</li>
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<li>B. Transonic wave drag of nose cones</li>
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<li>C. Streamer drag coefficient estimation</li>
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</ol>
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<h2>Resources</h2>
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<p>A list of useful technical rocketry resources is available in
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the <a href="http://wiki.openrocket.info/Resources">"Resources"
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wiki page</a>, including links to Barrowman's original report and
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thesis, extensions for the Barrowman method, experimental rocket
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data etc.</p>
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