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- <h1>Documentation for OpenRocket</h1>
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- <h2>User documentation</h2>
- <p>Unfortunately no user's guide currently exists for OpenRocket.
- Some documentation is available in the
- <a href="http://apps.sourceforge.net/mediawiki/openrocket/">OpenRocket
- wiki pages</a>, including a stub
- <a href="https://sourceforge.net/apps/mediawiki/openrocket/index.php?title=User%27s_Guide">User's
- guide</a> and a section of
- <a href="https://sourceforge.net/apps/mediawiki/openrocket/index.php?title=FAQ">frequently
- asked questions</a>.</p>
- <p>If you would like to help, please extend the documentation!</p>
- <h2>Technical documentation</h2>
- <p>OpenRocket was originally written as the Master's thesis of
- Sampo Niskanen at Helsinki University of Technology. The thesis
- currently functions as the technical documentation, and will be
- updated in the future to account for further enhancements.
- The thesis is licensed under a
- <a rel="license" href="http://creativecommons.org/licenses/by-nd-nc/1.0/fi/deed.en">Creative Commons BY-NC-ND License</a>.</p>
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- <p><a href="thesis.pdf">Development of an Open Source model
- rocket simulation software</a> (PDF, 1.3MB)</p>
- <p class="quote"><strong>Table of contents:</strong></p>
- <ol class="toc">
- <li>1. Introduction</li>
- <li>2. Basics of model rocket flight</li>
- <li>3. Aerodynamic properties of model rockets</li>
- <li>4. Flight simulation</li>
- <li>5. The OpenRocket simulation software</li>
- <li>6. Comparison with experimental data</li>
- <li>7. Conclusion</li>
- </ol>
- <ol class="toc">
- <li>A. Nose cone and transition geometries</li>
- <li>B. Transonic wave drag of nose cones</li>
- <li>C. Streamer drag coefficient estimation</li>
- </ol>
- <h2>Resources</h2>
- <p>A list of useful technical rocketry resources is available in
- the <a href="https://sourceforge.net/apps/mediawiki/openrocket/index.php?title=Resources">"Resources"
- wiki page</a>, including links to Barrowman's original report and
- thesis, extensions for the Barrowman method, experimental rocket
- data etc.</p>
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