http://wiki.openrocket.info/index.php?action=history&feed=atom&title=Resources
Resources - Revision history
2026-04-24T23:41:28Z
Revision history for this page on the wiki
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http://wiki.openrocket.info/index.php?title=Resources&diff=34544&oldid=prev
Jddj at 03:30, 10 March 2021
2021-03-10T03:30:20Z
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<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://strives-uploads-prod.s3.us-gov-west-1.amazonaws.com/19670020031/19670020031.pdf?AWSAccessKeyId=AKIASEVSKC45ZTTM42XZ&Expires=1602657806&Signature=D1R5vk%2FyKOIlSFKNei7yjzPQWE4%3D Static stability investigation of a sounding-rocket vehicle at Mach numbers from 1.50 to 4.63]'', Donald Babb and Dennis Fuller, NASA-TN-D-4014, 1967.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://strives-uploads-prod.s3.us-gov-west-1.amazonaws.com/19670020031/19670020031.pdf?AWSAccessKeyId=AKIASEVSKC45ZTTM42XZ&Expires=1602657806&Signature=D1R5vk%2FyKOIlSFKNei7yjzPQWE4%3D Static stability investigation of a sounding-rocket vehicle at Mach numbers from 1.50 to 4.63]'', Donald Babb and Dennis Fuller, NASA-TN-D-4014, 1967.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Experimental data of a wind tunnel investigation of a sounding rocket at subsonic, transonic and supersonic velocities. Available on [http://ntrs.nasa.gov/ NTRS].</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Experimental data of a wind tunnel investigation of a sounding rocket at subsonic, transonic and supersonic velocities. Available on [http://ntrs.nasa.gov/ NTRS].</div></td></tr>
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<tr><td colspan="2" class="diff-side-deleted"></td><td class="diff-marker" data-marker="+"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div><ins style="font-weight: bold; text-decoration: none;"><div style="float: left;">[[Scripting with Python and JPype|&larr; Scripting with Python and JPype (Appendix E)]]</div></ins></div></td></tr>
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Jddj
http://wiki.openrocket.info/index.php?title=Resources&diff=34506&oldid=prev
Jddj at 02:23, 10 March 2021
2021-03-10T02:23:13Z
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<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div><div style="text-align: center;"></div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div><div style="text-align: center;"></div></td></tr>
<tr><td class="diff-marker" data-marker="−"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #ffe49c; vertical-align: top; white-space: pre-wrap;"><div><div style="float: left;">[[<del style="font-weight: bold; text-decoration: none;">Resources</del>|&larr; <del style="font-weight: bold; text-decoration: none;">Resources </del>(Appendix <del style="font-weight: bold; text-decoration: none;">F</del>)]]</div><div style="<del style="font-weight: bold; text-decoration: none;">clear</del>: <del style="font-weight: bold; text-decoration: none;">both</del>;"></div></div></td><td class="diff-marker" data-marker="+"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div><div style="float: left;">[[<ins style="font-weight: bold; text-decoration: none;">Scripting with Python and JPype</ins>|&larr; <ins style="font-weight: bold; text-decoration: none;">Scripting with Python and JPype </ins>(Appendix <ins style="font-weight: bold; text-decoration: none;">E</ins>)]]</div></div></td></tr>
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Jddj
http://wiki.openrocket.info/index.php?title=Resources&diff=34505&oldid=prev
Jddj at 02:20, 10 March 2021
2021-03-10T02:20:49Z
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<tr><td colspan="2" class="diff-side-deleted"></td><td class="diff-marker" data-marker="+"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div><ins style="font-weight: bold; text-decoration: none;"></div></ins></div></td></tr>
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<tr><td colspan="2" class="diff-side-deleted"></td><td class="diff-marker" data-marker="+"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div><ins style="font-weight: bold; text-decoration: none;">{{UserGuideHelp}}</ins></div></td></tr>
<tr><td colspan="2" class="diff-side-deleted"></td><td class="diff-marker" data-marker="+"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div><ins style="font-weight: bold; text-decoration: none;"></ins></div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>Below are resources that have been found useful in the analysis of model rockets. Many useful scientific aerodynamic articles and documents are available at the invaluable [http://ntrs.nasa.gov/ NASA Technical Resources Server (NTRS)].</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>Below are resources that have been found useful in the analysis of model rockets. Many useful scientific aerodynamic articles and documents are available at the invaluable [http://ntrs.nasa.gov/ NASA Technical Resources Server (NTRS)].</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><br></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><br></td></tr>
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Jddj
http://wiki.openrocket.info/index.php?title=Resources&diff=34148&oldid=prev
216.172.121.92 at 06:57, 14 October 2020
2020-10-14T06:57:17Z
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<td colspan="2" style="background-color: #fff; color: #202122; text-align: center;">Revision as of 06:57, 14 October 2020</td>
</tr><tr><td colspan="2" class="diff-lineno" id="mw-diff-left-l16">Line 16:</td>
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<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://catalog.hathitrust.org/Record/004201684?type%5B%5D=all&lookfor%5B%5D=Tactical%20missile%20design&ft= Tactical missile design]'', 2nd edition, Eugene L. Fleeman, AIAA, 2006.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://catalog.hathitrust.org/Record/004201684?type%5B%5D=all&lookfor%5B%5D=Tactical%20missile%20design&ft= Tactical missile design]'', 2nd edition, Eugene L. Fleeman, AIAA, 2006.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Useful approximation methods for estimating the aerodynamic properties of rockets.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Useful approximation methods for estimating the aerodynamic properties of rockets.</div></td></tr>
<tr><td class="diff-marker" data-marker="−"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #ffe49c; vertical-align: top; white-space: pre-wrap;"><div>: ''[<del style="font-weight: bold; text-decoration: none;">http</del>://www.<del style="font-weight: bold; text-decoration: none;">aoe</del>.<del style="font-weight: bold; text-decoration: none;">vt.edu</del>/<del style="font-weight: bold; text-decoration: none;">~mason</del>/<del style="font-weight: bold; text-decoration: none;">Mason_f</del>/<del style="font-weight: bold; text-decoration: none;">CAtxtTop</del>.<del style="font-weight: bold; text-decoration: none;">html </del>Applied Computational Aerodynamics]'', William Mason.</div></td><td class="diff-marker" data-marker="+"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div>: ''[<ins style="font-weight: bold; text-decoration: none;">https</ins>://www.<ins style="font-weight: bold; text-decoration: none;">cambridge</ins>.<ins style="font-weight: bold; text-decoration: none;">org/us/academic/subjects</ins>/<ins style="font-weight: bold; text-decoration: none;">engineering</ins>/<ins style="font-weight: bold; text-decoration: none;">aerospace-engineering</ins>/<ins style="font-weight: bold; text-decoration: none;">applied-computational-aerodynamics-modern-engineering-approach?format=AR#33vGVwiCxYiDY74F</ins>.<ins style="font-weight: bold; text-decoration: none;">97 </ins>Applied Computational Aerodynamics]'', William Mason.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: An online textbook on computational aerodynamics.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: An online textbook on computational aerodynamics.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[http://mae-nas.eng.usu.edu/MAE_5900_Web/5900/USLI_2010/PDF_files/rocket_handbook.pdf Design of aerodynamically stabilized free rockets]'', MIL-HDBK-762, US Army Missile Command, 1990.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[http://mae-nas.eng.usu.edu/MAE_5900_Web/5900/USLI_2010/PDF_files/rocket_handbook.pdf Design of aerodynamically stabilized free rockets]'', MIL-HDBK-762, US Army Missile Command, 1990.</div></td></tr>
</table>
216.172.121.92
http://wiki.openrocket.info/index.php?title=Resources&diff=34147&oldid=prev
216.172.121.92 at 06:49, 14 October 2020
2020-10-14T06:49:14Z
<p></p>
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<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[http://www.aoe.vt.edu/~mason/Mason_f/CAtxtTop.html Applied Computational Aerodynamics]'', William Mason.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[http://www.aoe.vt.edu/~mason/Mason_f/CAtxtTop.html Applied Computational Aerodynamics]'', William Mason.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: An online textbook on computational aerodynamics.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: An online textbook on computational aerodynamics.</div></td></tr>
<tr><td class="diff-marker" data-marker="−"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #ffe49c; vertical-align: top; white-space: pre-wrap;"><div>: ''[http://<del style="font-weight: bold; text-decoration: none;">www</del>.<del style="font-weight: bold; text-decoration: none;">combatindex</del>.<del style="font-weight: bold; text-decoration: none;">com</del>/<del style="font-weight: bold; text-decoration: none;">mil_docs</del>/<del style="font-weight: bold; text-decoration: none;">pdf</del>/<del style="font-weight: bold; text-decoration: none;">hdbk</del>/<del style="font-weight: bold; text-decoration: none;">0700</del>/<del style="font-weight: bold; text-decoration: none;">MIL-HDBK-762</del>.pdf Design of aerodynamically stabilized free rockets]'', MIL-HDBK-762, US Army Missile Command, 1990.</div></td><td class="diff-marker" data-marker="+"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div>: ''[http://<ins style="font-weight: bold; text-decoration: none;">mae-nas.eng</ins>.<ins style="font-weight: bold; text-decoration: none;">usu</ins>.<ins style="font-weight: bold; text-decoration: none;">edu</ins>/<ins style="font-weight: bold; text-decoration: none;">MAE_5900_Web</ins>/<ins style="font-weight: bold; text-decoration: none;">5900</ins>/<ins style="font-weight: bold; text-decoration: none;">USLI_2010</ins>/<ins style="font-weight: bold; text-decoration: none;">PDF_files</ins>/<ins style="font-weight: bold; text-decoration: none;">rocket_handbook</ins>.pdf Design of aerodynamically stabilized free rockets]'', MIL-HDBK-762, US Army Missile Command, 1990.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Military handbook on the design of rockets, a good resource for aerodynamic estimation methods.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Military handbook on the design of rockets, a good resource for aerodynamic estimation methods.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: [http://www.thrustcurve.org/ ThrustCurve.org], John Coker.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: [http://www.thrustcurve.org/ ThrustCurve.org], John Coker.</div></td></tr>
</table>
216.172.121.92
http://wiki.openrocket.info/index.php?title=Resources&diff=34146&oldid=prev
216.172.121.92 at 06:46, 14 October 2020
2020-10-14T06:46:39Z
<p></p>
<table style="background-color: #fff; color: #202122;" data-mw="interface">
<col class="diff-marker" />
<col class="diff-content" />
<col class="diff-marker" />
<col class="diff-content" />
<tr class="diff-title" lang="en">
<td colspan="2" style="background-color: #fff; color: #202122; text-align: center;">← Older revision</td>
<td colspan="2" style="background-color: #fff; color: #202122; text-align: center;">Revision as of 06:46, 14 October 2020</td>
</tr><tr><td colspan="2" class="diff-lineno" id="mw-diff-left-l22">Line 22:</td>
<td colspan="2" class="diff-lineno">Line 22:</td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: [http://www.thrustcurve.org/ ThrustCurve.org], John Coker.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: [http://www.thrustcurve.org/ ThrustCurve.org], John Coker.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: An excellent resource for model rocket motor thrust curves.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: An excellent resource for model rocket motor thrust curves.</div></td></tr>
<tr><td class="diff-marker" data-marker="−"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #ffe49c; vertical-align: top; white-space: pre-wrap;"><div>: ''[<del style="font-weight: bold; text-decoration: none;">http</del>://<del style="font-weight: bold; text-decoration: none;">ntrs</del>.<del style="font-weight: bold; text-decoration: none;">nasa</del>.gov/<del style="font-weight: bold; text-decoration: none;">search</del>.<del style="font-weight: bold; text-decoration: none;">jsp</del>?<del style="font-weight: bold; text-decoration: none;">Ntk</del>=<del style="font-weight: bold; text-decoration: none;">all</del>&<del style="font-weight: bold; text-decoration: none;">Ntx</del>=<del style="font-weight: bold; text-decoration: none;">mode+matchall</del>&<del style="font-weight: bold; text-decoration: none;">Ntt</del>=<del style="font-weight: bold; text-decoration: none;">NASA-TN-D-4013 </del>Static stability investigation of a single-stage sounding rocket at Mach numbers from 0.60 to 1.20]'', James Ferris, NASA-TN-D-4013, 1967.</div></td><td class="diff-marker" data-marker="+"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div>: ''[<ins style="font-weight: bold; text-decoration: none;">https</ins>://<ins style="font-weight: bold; text-decoration: none;">strives-uploads-prod</ins>.<ins style="font-weight: bold; text-decoration: none;">s3</ins>.<ins style="font-weight: bold; text-decoration: none;">us-</ins>gov<ins style="font-weight: bold; text-decoration: none;">-west-1.amazonaws.com</ins>/<ins style="font-weight: bold; text-decoration: none;">19670020050/19670020050</ins>.<ins style="font-weight: bold; text-decoration: none;">pdf</ins>?<ins style="font-weight: bold; text-decoration: none;">AWSAccessKeyId</ins>=<ins style="font-weight: bold; text-decoration: none;">AKIASEVSKC45ZTTM42XZ</ins>&<ins style="font-weight: bold; text-decoration: none;">Expires</ins>=<ins style="font-weight: bold; text-decoration: none;">1602657948</ins>&<ins style="font-weight: bold; text-decoration: none;">Signature</ins>=<ins style="font-weight: bold; text-decoration: none;">%2Bii5hE%2FcD1g6ye3p3QUgsPF3Geo%3D </ins>Static stability investigation of a single-stage sounding rocket at Mach numbers from 0.60 to 1.20]'', James Ferris, NASA-TN-D-4013, 1967.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://strives-uploads-prod.s3.us-gov-west-1.amazonaws.com/19670020031/19670020031.pdf?AWSAccessKeyId=AKIASEVSKC45ZTTM42XZ&Expires=1602657806&Signature=D1R5vk%2FyKOIlSFKNei7yjzPQWE4%3D Static stability investigation of a sounding-rocket vehicle at Mach numbers from 1.50 to 4.63]'', Donald Babb and Dennis Fuller, NASA-TN-D-4014, 1967.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://strives-uploads-prod.s3.us-gov-west-1.amazonaws.com/19670020031/19670020031.pdf?AWSAccessKeyId=AKIASEVSKC45ZTTM42XZ&Expires=1602657806&Signature=D1R5vk%2FyKOIlSFKNei7yjzPQWE4%3D Static stability investigation of a sounding-rocket vehicle at Mach numbers from 1.50 to 4.63]'', Donald Babb and Dennis Fuller, NASA-TN-D-4014, 1967.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Experimental data of a wind tunnel investigation of a sounding rocket at subsonic, transonic and supersonic velocities. Available on [http://ntrs.nasa.gov/ NTRS].</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Experimental data of a wind tunnel investigation of a sounding rocket at subsonic, transonic and supersonic velocities. Available on [http://ntrs.nasa.gov/ NTRS].</div></td></tr>
</table>
216.172.121.92
http://wiki.openrocket.info/index.php?title=Resources&diff=34145&oldid=prev
216.172.121.92 at 06:44, 14 October 2020
2020-10-14T06:44:50Z
<p></p>
<table style="background-color: #fff; color: #202122;" data-mw="interface">
<col class="diff-marker" />
<col class="diff-content" />
<col class="diff-marker" />
<col class="diff-content" />
<tr class="diff-title" lang="en">
<td colspan="2" style="background-color: #fff; color: #202122; text-align: center;">← Older revision</td>
<td colspan="2" style="background-color: #fff; color: #202122; text-align: center;">Revision as of 06:44, 14 October 2020</td>
</tr><tr><td colspan="2" class="diff-lineno" id="mw-diff-left-l23">Line 23:</td>
<td colspan="2" class="diff-lineno">Line 23:</td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: An excellent resource for model rocket motor thrust curves.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: An excellent resource for model rocket motor thrust curves.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[http://ntrs.nasa.gov/search.jsp?Ntk=all&Ntx=mode+matchall&Ntt=NASA-TN-D-4013 Static stability investigation of a single-stage sounding rocket at Mach numbers from 0.60 to 1.20]'', James Ferris, NASA-TN-D-4013, 1967.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[http://ntrs.nasa.gov/search.jsp?Ntk=all&Ntx=mode+matchall&Ntt=NASA-TN-D-4013 Static stability investigation of a single-stage sounding rocket at Mach numbers from 0.60 to 1.20]'', James Ferris, NASA-TN-D-4013, 1967.</div></td></tr>
<tr><td class="diff-marker" data-marker="−"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #ffe49c; vertical-align: top; white-space: pre-wrap;"><div>: ''[<del style="font-weight: bold; text-decoration: none;">http</del>://<del style="font-weight: bold; text-decoration: none;">ntrs</del>.<del style="font-weight: bold; text-decoration: none;">nasa</del>.gov/<del style="font-weight: bold; text-decoration: none;">search</del>.<del style="font-weight: bold; text-decoration: none;">jsp</del>?<del style="font-weight: bold; text-decoration: none;">Ntk</del>=<del style="font-weight: bold; text-decoration: none;">all</del>&<del style="font-weight: bold; text-decoration: none;">Ntx</del>=<del style="font-weight: bold; text-decoration: none;">mode+matchall</del>&<del style="font-weight: bold; text-decoration: none;">Ntt</del>=<del style="font-weight: bold; text-decoration: none;">NASA-TN-D-4014 </del>Static stability investigation of a sounding-rocket vehicle at Mach numbers from 1.50 to 4.63]'', Donald Babb and Dennis Fuller, NASA-TN-D-4014, 1967.</div></td><td class="diff-marker" data-marker="+"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div>: ''[<ins style="font-weight: bold; text-decoration: none;">https</ins>://<ins style="font-weight: bold; text-decoration: none;">strives-uploads-prod</ins>.<ins style="font-weight: bold; text-decoration: none;">s3</ins>.<ins style="font-weight: bold; text-decoration: none;">us-</ins>gov<ins style="font-weight: bold; text-decoration: none;">-west-1.amazonaws.com</ins>/<ins style="font-weight: bold; text-decoration: none;">19670020031/19670020031</ins>.<ins style="font-weight: bold; text-decoration: none;">pdf</ins>?<ins style="font-weight: bold; text-decoration: none;">AWSAccessKeyId</ins>=<ins style="font-weight: bold; text-decoration: none;">AKIASEVSKC45ZTTM42XZ</ins>&<ins style="font-weight: bold; text-decoration: none;">Expires</ins>=<ins style="font-weight: bold; text-decoration: none;">1602657806</ins>&<ins style="font-weight: bold; text-decoration: none;">Signature</ins>=<ins style="font-weight: bold; text-decoration: none;">D1R5vk%2FyKOIlSFKNei7yjzPQWE4%3D </ins>Static stability investigation of a sounding-rocket vehicle at Mach numbers from 1.50 to 4.63]'', Donald Babb and Dennis Fuller, NASA-TN-D-4014, 1967.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Experimental data of a wind tunnel investigation of a sounding rocket at subsonic, transonic and supersonic velocities. Available on [http://ntrs.nasa.gov/ NTRS].</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Experimental data of a wind tunnel investigation of a sounding rocket at subsonic, transonic and supersonic velocities. Available on [http://ntrs.nasa.gov/ NTRS].</div></td></tr>
</table>
216.172.121.92
http://wiki.openrocket.info/index.php?title=Resources&diff=34144&oldid=prev
216.172.121.92 at 06:13, 14 October 2020
2020-10-14T06:13:18Z
<p></p>
<table style="background-color: #fff; color: #202122;" data-mw="interface">
<col class="diff-marker" />
<col class="diff-content" />
<col class="diff-marker" />
<col class="diff-content" />
<tr class="diff-title" lang="en">
<td colspan="2" style="background-color: #fff; color: #202122; text-align: center;">← Older revision</td>
<td colspan="2" style="background-color: #fff; color: #202122; text-align: center;">Revision as of 06:13, 14 October 2020</td>
</tr><tr><td colspan="2" class="diff-lineno" id="mw-diff-left-l14">Line 14:</td>
<td colspan="2" class="diff-lineno">Line 14:</td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://babel.hathitrust.org/cgi/pt?id=uc1.31822023531411&view=1up&seq=5 Fluid-dynamic drag]'' and ''[https://catalog.hathitrust.org/Record/006957952?type%5B%5D=all&lookfor%5B%5D=fluid-dynamic%20lift&ft= Fluid-dynamic lift]'', Sighard Hoerner, published by the author, 1965 & 1975.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://babel.hathitrust.org/cgi/pt?id=uc1.31822023531411&view=1up&seq=5 Fluid-dynamic drag]'' and ''[https://catalog.hathitrust.org/Record/006957952?type%5B%5D=all&lookfor%5B%5D=fluid-dynamic%20lift&ft= Fluid-dynamic lift]'', Sighard Hoerner, published by the author, 1965 & 1975.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Two compendiums of all wisdom and knowledge. Contains extensive gatherings of experimental data and compact explanations of the aerodynamic effects. Available as reprint editions.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Two compendiums of all wisdom and knowledge. Contains extensive gatherings of experimental data and compact explanations of the aerodynamic effects. Available as reprint editions.</div></td></tr>
<tr><td class="diff-marker" data-marker="−"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #ffe49c; vertical-align: top; white-space: pre-wrap;"><div>: ''Tactical missile design'', 2nd edition, Eugene L. Fleeman, AIAA, 2006.</div></td><td class="diff-marker" data-marker="+"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div>: ''<ins style="font-weight: bold; text-decoration: none;">[https://catalog.hathitrust.org/Record/004201684?type%5B%5D=all&lookfor%5B%5D=Tactical%20missile%20design&ft= </ins>Tactical missile design<ins style="font-weight: bold; text-decoration: none;">]</ins>'', 2nd edition, Eugene L. Fleeman, AIAA, 2006.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Useful approximation methods for estimating the aerodynamic properties of rockets.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Useful approximation methods for estimating the aerodynamic properties of rockets.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[http://www.aoe.vt.edu/~mason/Mason_f/CAtxtTop.html Applied Computational Aerodynamics]'', William Mason.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[http://www.aoe.vt.edu/~mason/Mason_f/CAtxtTop.html Applied Computational Aerodynamics]'', William Mason.</div></td></tr>
</table>
216.172.121.92
http://wiki.openrocket.info/index.php?title=Resources&diff=34143&oldid=prev
216.172.121.92 at 06:08, 14 October 2020
2020-10-14T06:08:33Z
<p></p>
<table style="background-color: #fff; color: #202122;" data-mw="interface">
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<col class="diff-marker" />
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<tr class="diff-title" lang="en">
<td colspan="2" style="background-color: #fff; color: #202122; text-align: center;">← Older revision</td>
<td colspan="2" style="background-color: #fff; color: #202122; text-align: center;">Revision as of 06:08, 14 October 2020</td>
</tr><tr><td colspan="2" class="diff-lineno" id="mw-diff-left-l12">Line 12:</td>
<td colspan="2" class="diff-lineno">Line 12:</td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://dspace.mit.edu/handle/1721.1/1701/restricted-resource?bitstreamId=b112dcb2-af18-41f5-aeaf-3525c7bfe318 Topics in Advanced Model Rocketry]'', Mandell, Caporaso, Bengen, MIT Press, 1973.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://dspace.mit.edu/handle/1721.1/1701/restricted-resource?bitstreamId=b112dcb2-af18-41f5-aeaf-3525c7bfe318 Topics in Advanced Model Rocketry]'', Mandell, Caporaso, Bengen, MIT Press, 1973.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: An excellent theoretical study on the flight of model rockets. Available as a reprint edition.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: An excellent theoretical study on the flight of model rockets. Available as a reprint edition.</div></td></tr>
<tr><td class="diff-marker" data-marker="−"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #ffe49c; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://babel.hathitrust.org/cgi/pt?id=uc1.31822023531411&view=1up&seq=5 Fluid-dynamic drag]'' and ''Fluid-dynamic lift'', Sighard Hoerner, published by the author, 1965 & 1975.</div></td><td class="diff-marker" data-marker="+"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://babel.hathitrust.org/cgi/pt?id=uc1.31822023531411&view=1up&seq=5 Fluid-dynamic drag]'' and ''<ins style="font-weight: bold; text-decoration: none;">[https://catalog.hathitrust.org/Record/006957952?type%5B%5D=all&lookfor%5B%5D=fluid-dynamic%20lift&ft= </ins>Fluid-dynamic lift<ins style="font-weight: bold; text-decoration: none;">]</ins>'', Sighard Hoerner, published by the author, 1965 & 1975.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Two compendiums of all wisdom and knowledge. Contains extensive gatherings of experimental data and compact explanations of the aerodynamic effects. Available as reprint editions.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Two compendiums of all wisdom and knowledge. Contains extensive gatherings of experimental data and compact explanations of the aerodynamic effects. Available as reprint editions.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''Tactical missile design'', 2nd edition, Eugene L. Fleeman, AIAA, 2006.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''Tactical missile design'', 2nd edition, Eugene L. Fleeman, AIAA, 2006.</div></td></tr>
</table>
216.172.121.92
http://wiki.openrocket.info/index.php?title=Resources&diff=34142&oldid=prev
216.172.121.92 at 05:58, 14 October 2020
2020-10-14T05:58:48Z
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<td colspan="2" style="background-color: #fff; color: #202122; text-align: center;">← Older revision</td>
<td colspan="2" style="background-color: #fff; color: #202122; text-align: center;">Revision as of 05:58, 14 October 2020</td>
</tr><tr><td colspan="2" class="diff-lineno" id="mw-diff-left-l12">Line 12:</td>
<td colspan="2" class="diff-lineno">Line 12:</td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://dspace.mit.edu/handle/1721.1/1701/restricted-resource?bitstreamId=b112dcb2-af18-41f5-aeaf-3525c7bfe318 Topics in Advanced Model Rocketry]'', Mandell, Caporaso, Bengen, MIT Press, 1973.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''[https://dspace.mit.edu/handle/1721.1/1701/restricted-resource?bitstreamId=b112dcb2-af18-41f5-aeaf-3525c7bfe318 Topics in Advanced Model Rocketry]'', Mandell, Caporaso, Bengen, MIT Press, 1973.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: An excellent theoretical study on the flight of model rockets. Available as a reprint edition.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: An excellent theoretical study on the flight of model rockets. Available as a reprint edition.</div></td></tr>
<tr><td class="diff-marker" data-marker="−"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #ffe49c; vertical-align: top; white-space: pre-wrap;"><div>: ''Fluid-dynamic drag'' and ''Fluid-dynamic lift'', Sighard Hoerner, published by the author, 1965 & 1975.</div></td><td class="diff-marker" data-marker="+"></td><td style="color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div>: ''<ins style="font-weight: bold; text-decoration: none;">[https://babel.hathitrust.org/cgi/pt?id=uc1.31822023531411&view=1up&seq=5 </ins>Fluid-dynamic drag<ins style="font-weight: bold; text-decoration: none;">]</ins>'' and ''Fluid-dynamic lift'', Sighard Hoerner, published by the author, 1965 & 1975.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Two compendiums of all wisdom and knowledge. Contains extensive gatherings of experimental data and compact explanations of the aerodynamic effects. Available as reprint editions.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>:: Two compendiums of all wisdom and knowledge. Contains extensive gatherings of experimental data and compact explanations of the aerodynamic effects. Available as reprint editions.</div></td></tr>
<tr><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''Tactical missile design'', 2nd edition, Eugene L. Fleeman, AIAA, 2006.</div></td><td class="diff-marker"></td><td style="background-color: #f8f9fa; color: #202122; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #eaecf0; vertical-align: top; white-space: pre-wrap;"><div>: ''Tactical missile design'', 2nd edition, Eugene L. Fleeman, AIAA, 2006.</div></td></tr>
</table>
216.172.121.92