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	<id>https://mediawiki.aerodecelerator.org/index.php?action=history&amp;feed=atom&amp;title=Parachute_Performance</id>
	<title>Parachute Performance - Revision history</title>
	<link rel="self" type="application/atom+xml" href="https://mediawiki.aerodecelerator.org/index.php?action=history&amp;feed=atom&amp;title=Parachute_Performance"/>
	<link rel="alternate" type="text/html" href="https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;action=history"/>
	<updated>2026-05-21T01:00:22Z</updated>
	<subtitle>Revision history for this page on the wiki</subtitle>
	<generator>MediaWiki 1.41.0</generator>
	<entry>
		<id>https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=737&amp;oldid=prev</id>
		<title>Parachute at 17:14, 26 June 2024</title>
		<link rel="alternate" type="text/html" href="https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=737&amp;oldid=prev"/>
		<updated>2024-06-26T17:14:01Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;table style=&quot;background-color: #fff; color: #202122;&quot; data-mw=&quot;interface&quot;&gt;
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				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 17:14, 26 June 2024&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l1511&quot;&gt;Line 1,511:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 1,511:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.166. U.S. Air Force. Extraction Parachute Clustering Techniques, by C. W Marshall. USAF, October 1958. (USAF Report FTC-TN-58-18.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.166. U.S. Air Force. Extraction Parachute Clustering Techniques, by C. W Marshall. USAF, October 1958. (USAF Report FTC-TN-58-18.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.167. &lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;-&lt;/del&gt;. G-12B 64-Ft Cargo Parachute Cluster Tests, by C. W Marshall. USAF, March 1958. (USAF Report FTC-LR-58-102.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.167. &lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;_____&lt;/ins&gt;. G-12B 64-Ft Cargo Parachute Cluster Tests, by C. W Marshall. USAF, March 1958. (USAF Report FTC-LR-58-102.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.168. &lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;-&lt;/del&gt;. G-11, A Parachute Retardation System, by I. Svoboda. USAF, February 1961. (USAF Report FTC-TN-61-102.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.168. &lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;_____&lt;/ins&gt;.G-11, A Parachute Retardation System, by I. Svoboda. USAF, February 1961. (USAF Report FTC-TN-61-102.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.169. W C. Buhler. &amp;quot;Development of a High Performance Ringsail Parachute Cluster.&amp;quot; AIAA Paper, May 1973. (AIAA 73-468.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.169. W C. Buhler. &amp;quot;Development of a High Performance Ringsail Parachute Cluster.&amp;quot; AIAA Paper, May 1973. (AIAA 73-468.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/table&gt;</summary>
		<author><name>Parachute</name></author>
	</entry>
	<entry>
		<id>https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=736&amp;oldid=prev</id>
		<title>Parachute at 16:17, 26 June 2024</title>
		<link rel="alternate" type="text/html" href="https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=736&amp;oldid=prev"/>
		<updated>2024-06-26T16:17:07Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;table style=&quot;background-color: #fff; color: #202122;&quot; data-mw=&quot;interface&quot;&gt;
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				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 16:17, 26 June 2024&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l1401&quot;&gt;Line 1,401:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 1,401:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.111. R J. Bobbitt, R. J. Mayhue, G. L. Faurote, and L. L. Galigher. &amp;quot;Supersonic and Subsonic Wind Tunnel Tests on Reefed and Unreefed Disk-Gap-Band Parachutes.&amp;quot; AIAA Paper, September 1970. (AIAA 70-1172.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.111. R J. Bobbitt, R. J. Mayhue, G. L. Faurote, and L. L. Galigher. &amp;quot;Supersonic and Subsonic Wind Tunnel Tests on Reefed and Unreefed Disk-Gap-Band Parachutes.&amp;quot; AIAA Paper, September 1970. (AIAA 70-1172.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.112. D. F Wolf and R. H. Croll. &quot;Wind &lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;'l'nnel &lt;/del&gt;Measurements of Dynamic Reefing Line Tension in Ribbon Parachutes.&quot; AIAA Paper, March 1979. (AIAA 79-465.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.112. D. F Wolf and R. H. Croll. &quot;Wind &lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Tunnel &lt;/ins&gt;Measurements of Dynamic Reefing Line Tension in Ribbon Parachutes.&quot; AIAA Paper, March 1979. (AIAA 79-465.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.113. U.S. Air Force. Reefing of Parachutes-Forces in Reefing Line, by T W Knacke. USAF, October 1981. (USAF Report ASD-TR-81-5029.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.113. U.S. Air Force. Reefing of Parachutes-Forces in Reefing Line, by T W Knacke. USAF, October 1981. (USAF Report ASD-TR-81-5029.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l1409&quot;&gt;Line 1,409:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 1,409:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.115. U.S. Air Force. Pressure Distribution During Parachute Inflation Phase I, Infinite Mass Opening Case, by H. D. Melzig and P. K. Schmidt. USAF, March 1966. (USAF Report AFFDL-TR-66-110.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.115. U.S. Air Force. Pressure Distribution During Parachute Inflation Phase I, Infinite Mass Opening Case, by H. D. Melzig and P. K. Schmidt. USAF, March 1966. (USAF Report AFFDL-TR-66-110.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.116&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;. &lt;/del&gt;.Pressure Distribution During Parachute Opening, by H. D. Melzig and C. Salaris. USAF, February 1969. (USAF Report AFFDL-TR-68-135.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.116. Pressure Distribution During Parachute Opening, by H. D. Melzig and C. Salaris. USAF, February 1969. (USAF Report AFFDL-TR-68-135.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.117. Sandia National Laboratories. Pressure and Profile Data of 20* Conical Ribbon Parachutes, Volumes I and 11, by H. G. Heinrich. SNL, May 1977. (SNL Report 77-7005.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.117. Sandia National Laboratories. Pressure and Profile Data of 20* Conical Ribbon Parachutes, Volumes I and 11, by H. G. Heinrich. SNL, May 1977. (SNL Report 77-7005.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l1419&quot;&gt;Line 1,419:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 1,419:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.120. K. K. Muramoto and W L. Garrard. &amp;quot;Method for Calculating the Pressure Field About a Ribbon Parachute Canopy in Steady Descent.&amp;quot; AIAA Paper, September 1984. (AIAA 84-0794.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.120. K. K. Muramoto and W L. Garrard. &amp;quot;Method for Calculating the Pressure Field About a Ribbon Parachute Canopy in Steady Descent.&amp;quot; AIAA Paper, September 1984. (AIAA 84-0794.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.121. U.S. Air Force. Recovery &lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Systerms &lt;/del&gt;for Missiles and Target Aircraft, by J. R. Downing, J. H. McClow, R. 0. Fredette, and H. V. Hawkins. Part I, I, and III. USAF, March 1954 to December 1958. (USAF Report TR-58-53.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.121. U.S. Air Force. Recovery &lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Systems &lt;/ins&gt;for Missiles and Target Aircraft, by J. R. Downing, J. H. McClow, R. 0. Fredette, and H. V. Hawkins. Part I, I, and III. USAF, March 1954 to December 1958. (USAF Report TR-58-53.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.122. _____. Study of Parachute Performance and Design Parameters for High Dynamic Pressure Operation, by P. F Pederson. USAF, May 1964. (USAF Report FDL-TDR-64-66.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.122. _____. Study of Parachute Performance and Design Parameters for High Dynamic Pressure Operation, by P. F Pederson. USAF, May 1964. (USAF Report FDL-TDR-64-66.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/table&gt;</summary>
		<author><name>Parachute</name></author>
	</entry>
	<entry>
		<id>https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=735&amp;oldid=prev</id>
		<title>Parachute at 16:10, 26 June 2024</title>
		<link rel="alternate" type="text/html" href="https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=735&amp;oldid=prev"/>
		<updated>2024-06-26T16:10:19Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;table style=&quot;background-color: #fff; color: #202122;&quot; data-mw=&quot;interface&quot;&gt;
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				&lt;col class=&quot;diff-content&quot; /&gt;
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				&lt;tr class=&quot;diff-title&quot; lang=&quot;en&quot;&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 16:10, 26 June 2024&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l49&quot;&gt;Line 49:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 49:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-10. Sixty-Four-Foot-Diameter Merucry Ringsail Parachute.2.jpg|center|thumb|682x682px|FIGURE 5-10. Sixty-Four-Foot-Diameter Mercury Ringsail Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-10. Sixty-Four-Foot-Diameter Merucry Ringsail Parachute.2.jpg|center|thumb|682x682px|FIGURE 5-10. Sixty-Four-Foot-Diameter Mercury Ringsail Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-11. Rotofoil Parachute..jpg|center|thumb|517x517px|FIGURE 5-11. Rotofoil Parachute]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-11. Rotofoil Parachute..jpg|center|thumb|517x517px|FIGURE 5-11. Rotofoil Parachute]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-12. Vortex Ring Parachute (Only Two of Four Adjacent Gores are Shown)..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;600x600px&lt;/del&gt;|FIGURE 5-12. Vortex Ring Parachute (Only Two of Four Adjacent Gores are Shown).]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-12. Vortex Ring Parachute (Only Two of Four Adjacent Gores are Shown)..jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;442x442px&lt;/ins&gt;|FIGURE 5-12. Vortex Ring Parachute (Only Two of Four Adjacent Gores are Shown)&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;.]]&lt;/ins&gt;&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-14. Hi-Glide (Maneuverable) Parachutes..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;761x761px&lt;/del&gt;|FIGURE 5-14. Hi-Glide (Maneuverable) Parachutes.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;[[File:FIGURE 5-13. Thirty-Five-Foot-Diameter T-10 (MC1-1B) Paratrooper Parachute, Modified With Slots and Control Lines for Glide and Controllability.1.jpg|center|thumb|FIGURE 5-13. Thirty-Five-Foot-Diameter T-10 (MC1-1B) Paratrooper Parachute, Modified With Slots and Control Lines for Glide and Controllability&lt;/ins&gt;.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-15. Ballute (Ballon-Type Decelerator)..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;420x420px&lt;/del&gt;|FIGURE 5-15. Ballute (Ballon-Type Decelerator).]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-14. Hi-Glide (Maneuverable) Parachutes.&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;2&lt;/ins&gt;.jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;778x778px&lt;/ins&gt;|FIGURE 5-14. Hi-Glide (Maneuverable) Parachutes.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-side-deleted&quot;&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-15. Ballute (Ballon-Type Decelerator).&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;2&lt;/ins&gt;.jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;433x433px&lt;/ins&gt;|FIGURE 5-15. Ballute (Ballon-Type Decelerator).]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;==  5.2 PARACHUTE DRAG AND WAKE EFFECTS ==&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;==  5.2 PARACHUTE DRAG AND WAKE EFFECTS ==&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/table&gt;</summary>
		<author><name>Parachute</name></author>
	</entry>
	<entry>
		<id>https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=731&amp;oldid=prev</id>
		<title>Parachute at 14:34, 26 June 2024</title>
		<link rel="alternate" type="text/html" href="https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=731&amp;oldid=prev"/>
		<updated>2024-06-26T14:34:18Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;table style=&quot;background-color: #fff; color: #202122;&quot; data-mw=&quot;interface&quot;&gt;
				&lt;col class=&quot;diff-marker&quot; /&gt;
				&lt;col class=&quot;diff-content&quot; /&gt;
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				&lt;tr class=&quot;diff-title&quot; lang=&quot;en&quot;&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 14:34, 26 June 2024&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l49&quot;&gt;Line 49:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 49:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-10. Sixty-Four-Foot-Diameter Merucry Ringsail Parachute.2.jpg|center|thumb|682x682px|FIGURE 5-10. Sixty-Four-Foot-Diameter Mercury Ringsail Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-10. Sixty-Four-Foot-Diameter Merucry Ringsail Parachute.2.jpg|center|thumb|682x682px|FIGURE 5-10. Sixty-Four-Foot-Diameter Mercury Ringsail Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-11. Rotofoil Parachute..jpg|center|thumb|517x517px|FIGURE 5-11. Rotofoil Parachute]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-11. Rotofoil Parachute..jpg|center|thumb|517x517px|FIGURE 5-11. Rotofoil Parachute]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;13&lt;/del&gt;. &lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Thirty-Five-Foot-Diameter T-10 &lt;/del&gt;(&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;MC1-1B&lt;/del&gt;) &lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Paratrooper Parachute, Modified With Slots and Control Lines for Glide and Controllability&lt;/del&gt;..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;426x426px&lt;/del&gt;|FIGURE 5-&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;13&lt;/del&gt;. &lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Thirty-Five-Foot-Diameter T-10 &lt;/del&gt;(&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;MC1-1B&lt;/del&gt;) &lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Paratrooper Parachute, Modified With Slots and Control Lines for Glide and Controllability&lt;/del&gt;.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;12&lt;/ins&gt;. &lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Vortex Ring Parachute &lt;/ins&gt;(&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Only Two of Four Adjacent Gores are Shown&lt;/ins&gt;)..jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;600x600px&lt;/ins&gt;|FIGURE 5-&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;12&lt;/ins&gt;. &lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Vortex Ring Parachute &lt;/ins&gt;(&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Only Two of Four Adjacent Gores are Shown&lt;/ins&gt;).]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-14. Hi-Glide (Maneuverable) Parachutes..jpg|center|thumb|761x761px|FIGURE 5-14. Hi-Glide (Maneuverable) Parachutes.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-14. Hi-Glide (Maneuverable) Parachutes..jpg|center|thumb|761x761px|FIGURE 5-14. Hi-Glide (Maneuverable) Parachutes.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-15. Ballute (Ballon-Type Decelerator)..jpg|center|thumb|420x420px|FIGURE 5-15. Ballute (Ballon-Type Decelerator).]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-15. Ballute (Ballon-Type Decelerator)..jpg|center|thumb|420x420px|FIGURE 5-15. Ballute (Ballon-Type Decelerator).]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l96&quot;&gt;Line 96:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 96:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;Decreasing the porosity increases the drag coefficient but also produces a less stable parachute and a higher opening force.  &lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;Decreasing the porosity increases the drag coefficient but also produces a less stable parachute and a higher opening force.  &lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;Canopy profiles of quarter-spherical shapes and the similar tri conical shapes have shown the highest drag coefficients for circular canopy designs.&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;Canopy profiles of quarter-spherical shapes and the similar tri conical shapes have shown the highest drag coefficients for circular canopy designs.&amp;lt;nowiki&amp;gt;*&amp;lt;/nowiki&amp;gt; In this manual, &amp;lt;math&amp;gt;C_{D_o}S_o&amp;lt;/math&amp;gt;, and &amp;lt;math&amp;gt;(C_DS)_p&amp;lt;/math&amp;gt; are interchangeable.&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;&amp;lt;nowiki&amp;gt;*&amp;lt;/nowiki&amp;gt; In this manual, &amp;lt;math&amp;gt;C_{D_o}S_o&amp;lt;/math&amp;gt;, and &amp;lt;math&amp;gt;(C_DS)_p&amp;lt;/math&amp;gt; are interchangeable.&lt;/div&gt;&lt;/td&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-side-added&quot;&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;=== 5.2.1 Canopy Shape and Suspension Line Length Effects ===&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;=== 5.2.1 Canopy Shape and Suspension Line Length Effects ===&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;In 1949, the U.S. Air Force conducted model drop tests of 1600-square-inch parachutes under controlled conditions in the Lakehurst, New Jersey, airship hangar (Reference 5.1). These tests established several facts previously unknown or only suspected.  &lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;In 1949, the U.S. Air Force conducted model drop tests of 1600-square-inch parachutes under controlled conditions in the Lakehurst, New Jersey, airship hangar (Reference 5.1). These tests established several facts previously unknown or only suspected.  &lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;Solid textile parachutes of a round or cornered design and with a flat or shaped profile descended in a vertical line, but oscillated violently when dropped at rates of descent greater than 30 ft/s. The same parachutes, when dropped with a low weight, had a 10-ft/s rate of descent and descended in a stable, non oscillating attitude, but glided at angles up to 45 degrees. In the 15-to 25-ft/s descent range, these parachutes combined oscillation with straight descent, or with glide but no oscillation. Gliding resulted in a low vertical velocity component and a high drag coefficient. Vertical descent with oscillation at the higher rates of descent resulted in lower vertical drag coefficients.  &lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;Solid textile parachutes of a round or cornered design and with a flat or shaped profile descended in a vertical line, but oscillated violently when dropped at rates of descent greater than 30 ft/s. The same parachutes, when dropped with a low weight, had a 10-ft/s rate of descent and descended in a stable, non&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;-&lt;/ins&gt;oscillating attitude, but glided at angles up to 45 degrees. In the 15-to 25-ft/s descent range, these parachutes combined oscillation with straight descent, or with glide but no oscillation. Gliding resulted in a low vertical velocity component and a high drag coefficient. Vertical descent with oscillation at the higher rates of descent resulted in lower vertical drag coefficients.  &lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;For the same surface areas, conical and quarter-spherical canopies had higher drag coefficients than circular flat canopies. Figure 5-16 shows that, at a rate of descent of 20 ft/s, a 30-degree conical parachute has a 9.5% higher drag coefficient than a flat, circular canopy, and a quarter-spherical canopy has a 14.5% higher drag coefficient. These tests were the basis for the quarter-spherical profiles of the ringsail and the triconical parachute canopies.&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;For the same surface areas, conical and quarter-spherical canopies had higher drag coefficients than circular flat canopies. Figure 5-16 shows that, at a rate of descent of 20 ft/s, a 30-degree conical parachute has a 9.5% higher drag coefficient than a flat, circular canopy, and a quarter-spherical canopy has a 14.5% higher drag coefficient. These tests were the basis for the quarter-spherical profiles of the ringsail and the triconical parachute canopies.&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/table&gt;</summary>
		<author><name>Parachute</name></author>
	</entry>
	<entry>
		<id>https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=730&amp;oldid=prev</id>
		<title>Parachute at 14:28, 26 June 2024</title>
		<link rel="alternate" type="text/html" href="https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=730&amp;oldid=prev"/>
		<updated>2024-06-26T14:28:28Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;table style=&quot;background-color: #fff; color: #202122;&quot; data-mw=&quot;interface&quot;&gt;
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				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 14:28, 26 June 2024&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l47&quot;&gt;Line 47:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 47:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-8. Thirty-Two-Foot-Diameter Ribbon, Landing Deceleration Parachute.2.jpg|center|thumb|1067x1067px|FIGURE 5-8. Thirty-Two-Foot-Diameter Ribbon, Landing Deceleration Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-8. Thirty-Two-Foot-Diameter Ribbon, Landing Deceleration Parachute.2.jpg|center|thumb|1067x1067px|FIGURE 5-8. Thirty-Two-Foot-Diameter Ribbon, Landing Deceleration Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-9. Ringslot Parachute.2.jpg|center|thumb|1022x1022px|FIGURE 5-9. Ringslot Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-9. Ringslot Parachute.2.jpg|center|thumb|1022x1022px|FIGURE 5-9. Ringslot Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-10. Sixty-Four-Foot-Diameter Merucry Ringsail Parachute.2.jpg|center|thumb|682x682px|FIGURE 5-10. Sixty-Four-Foot-Diameter &lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Merucry &lt;/del&gt;Ringsail Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-10. Sixty-Four-Foot-Diameter Merucry Ringsail Parachute.2.jpg|center|thumb|682x682px|FIGURE 5-10. Sixty-Four-Foot-Diameter &lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Mercury &lt;/ins&gt;Ringsail Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-11. Rotofoil Parachute..jpg|center|thumb|517x517px|FIGURE 5-11. Rotofoil Parachute]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-11. Rotofoil Parachute..jpg|center|thumb|517x517px|FIGURE 5-11. Rotofoil Parachute]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;[[File:FIGURE 5-12. Vortex Ring Parachute (Only Two of Four Adjacent Gores are Shown)..jpg|center|thumb|442x442px|FIGURE 5-12. Vortex Ring Parachute (Only Two of Four Adjacent Gores are Shown).]]&lt;/del&gt;&lt;/div&gt;&lt;/td&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-side-added&quot;&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-13. Thirty-Five-Foot-Diameter T-10 (MC1-1B) Paratrooper Parachute, Modified With Slots and Control Lines for Glide and Controllability..jpg|center|thumb|426x426px|FIGURE 5-13. Thirty-Five-Foot-Diameter T-10 (MC1-1B) Paratrooper Parachute, Modified With Slots and Control Lines for Glide and Controllability.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-13. Thirty-Five-Foot-Diameter T-10 (MC1-1B) Paratrooper Parachute, Modified With Slots and Control Lines for Glide and Controllability..jpg|center|thumb|426x426px|FIGURE 5-13. Thirty-Five-Foot-Diameter T-10 (MC1-1B) Paratrooper Parachute, Modified With Slots and Control Lines for Glide and Controllability.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-14. Hi-Glide (Maneuverable) Parachutes..jpg|center|thumb|761x761px|FIGURE 5-14. Hi-Glide (Maneuverable) Parachutes.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-14. Hi-Glide (Maneuverable) Parachutes..jpg|center|thumb|761x761px|FIGURE 5-14. Hi-Glide (Maneuverable) Parachutes.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/table&gt;</summary>
		<author><name>Parachute</name></author>
	</entry>
	<entry>
		<id>https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=728&amp;oldid=prev</id>
		<title>Parachute at 14:18, 26 June 2024</title>
		<link rel="alternate" type="text/html" href="https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=728&amp;oldid=prev"/>
		<updated>2024-06-26T14:18:21Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;table style=&quot;background-color: #fff; color: #202122;&quot; data-mw=&quot;interface&quot;&gt;
				&lt;col class=&quot;diff-marker&quot; /&gt;
				&lt;col class=&quot;diff-content&quot; /&gt;
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				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 14:18, 26 June 2024&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l40&quot;&gt;Line 40:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 40:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-1. Twenty-Eight-Foot-Diameter Circular, Flat Personnel Parachute.2.jpg|center|thumb|582x582px|FIGURE 5-1. Twenty-Eight-Foot-Diameter Circular, Flat Personnel Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-1. Twenty-Eight-Foot-Diameter Circular, Flat Personnel Parachute.2.jpg|center|thumb|582x582px|FIGURE 5-1. Twenty-Eight-Foot-Diameter Circular, Flat Personnel Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-2. Two-Hundred-Foot-Diameter Circular, Flat Cargo Parachute.2.jpg|center|thumb|524x524px|FIGURE 5-2. Two-Hundred-Foot-Diameter Circular, Flat Cargo Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-2. Two-Hundred-Foot-Diameter Circular, Flat Cargo Parachute.2.jpg|center|thumb|524x524px|FIGURE 5-2. Two-Hundred-Foot-Diameter Circular, Flat Cargo Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-3. Army Paratrooper 35-Foot-Diameter Extended-Skirt Parachute..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;404x404px&lt;/del&gt;|FIGURE 5-3. Army Paratrooper 35-Foot-Diameter Extended-Skirt Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-3. Army Paratrooper 35-Foot-Diameter Extended-Skirt Parachute.&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;2&lt;/ins&gt;.jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;654x654px&lt;/ins&gt;|FIGURE 5-3. Army Paratrooper 35-Foot-Diameter Extended-Skirt Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-4. Twenty-Four-Foot-Diameter Hemispherical Parachute..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;405x405px&lt;/del&gt;|FIGURE 5-4. Twenty-Four-Foot-Diameter Hemispherical Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-4. Twenty-Four-Foot-Diameter Hemispherical Parachute.&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;2&lt;/ins&gt;.jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;651x651px&lt;/ins&gt;|FIGURE 5-4. Twenty-Four-Foot-Diameter Hemispherical Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-5. Guide Surface Parachute..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;616x616px&lt;/del&gt;|FIGURE 5-5. Guide Surface Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-5. Guide Surface Parachute.&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;2&lt;/ins&gt;.jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;994x994px&lt;/ins&gt;|FIGURE 5-5. Guide Surface Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-6. Seventy-Foot-Diameter Annular Parachute With 24-Foot-Diameter Engagement Parachute in Midair Retrieval Configuration..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;467x467px&lt;/del&gt;|FIGURE 5-6. Seventy-Foot-Diameter Annular Parachute With 24-Foot-Diameter Engagement Parachute in Midair Retrieval Configuration.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-6. Seventy-Foot-Diameter Annular Parachute With 24-Foot-Diameter Engagement Parachute in Midair Retrieval Configuration.&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;2&lt;/ins&gt;.jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;760x760px&lt;/ins&gt;|FIGURE 5-6. Seventy-Foot-Diameter Annular Parachute With 24-Foot-Diameter Engagement Parachute in Midair Retrieval Configuration.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-7. Cross Parachute in Wind-Tunnel Test..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;329x329px&lt;/del&gt;|FIGURE 5-7. Cross Parachute in Wind-Tunnel Test.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-7. Cross Parachute in Wind-Tunnel Test.&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;2&lt;/ins&gt;.jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;495x495px&lt;/ins&gt;|FIGURE 5-7. Cross Parachute in Wind-Tunnel Test.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-8. Thirty-Two-Foot-Diameter Ribbon, Landing Deceleration Parachute..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;680x680px&lt;/del&gt;|FIGURE 5-8. Thirty-Two-Foot-Diameter Ribbon, Landing Deceleration Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-8. Thirty-Two-Foot-Diameter Ribbon, Landing Deceleration Parachute.&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;2&lt;/ins&gt;.jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;1067x1067px&lt;/ins&gt;|FIGURE 5-8. Thirty-Two-Foot-Diameter Ribbon, Landing Deceleration Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-9. Ringslot Parachute..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;624x624px&lt;/del&gt;|FIGURE 5-9. Ringslot Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-9. Ringslot Parachute.&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;2&lt;/ins&gt;.jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;1022x1022px&lt;/ins&gt;|FIGURE 5-9. Ringslot Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-10. Sixty-Four-Foot-Diameter &lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Mercury &lt;/del&gt;Ringsail Parachute..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;494x494px&lt;/del&gt;|FIGURE 5-10. Sixty-Four-Foot-Diameter &lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Mercury &lt;/del&gt;Ringsail Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-10. Sixty-Four-Foot-Diameter &lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Merucry &lt;/ins&gt;Ringsail Parachute.&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;2&lt;/ins&gt;.jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;682x682px&lt;/ins&gt;|FIGURE 5-10. Sixty-Four-Foot-Diameter &lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Merucry &lt;/ins&gt;Ringsail Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-11. Rotofoil Parachute..jpg|center|thumb|517x517px|FIGURE 5-11. Rotofoil Parachute]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-11. Rotofoil Parachute..jpg|center|thumb|517x517px|FIGURE 5-11. Rotofoil Parachute]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-12. Vortex Ring Parachute (Only Two of Four Adjacent Gores are Shown)..jpg|center|thumb|442x442px|FIGURE 5-12. Vortex Ring Parachute (Only Two of Four Adjacent Gores are Shown).]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-12. Vortex Ring Parachute (Only Two of Four Adjacent Gores are Shown)..jpg|center|thumb|442x442px|FIGURE 5-12. Vortex Ring Parachute (Only Two of Four Adjacent Gores are Shown).]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/table&gt;</summary>
		<author><name>Parachute</name></author>
	</entry>
	<entry>
		<id>https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=719&amp;oldid=prev</id>
		<title>Parachute at 23:05, 25 June 2024</title>
		<link rel="alternate" type="text/html" href="https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=719&amp;oldid=prev"/>
		<updated>2024-06-25T23:05:00Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;table style=&quot;background-color: #fff; color: #202122;&quot; data-mw=&quot;interface&quot;&gt;
				&lt;col class=&quot;diff-marker&quot; /&gt;
				&lt;col class=&quot;diff-content&quot; /&gt;
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				&lt;tr class=&quot;diff-title&quot; lang=&quot;en&quot;&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 23:05, 25 June 2024&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l38&quot;&gt;Line 38:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 38:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;Note: Maneuverable parachutes with a glide ratio L/D of 2.5 or better have been defined in the literature as &amp;quot;hi-glide parachutes.&amp;quot; This includes the parawing, the parafoil, the sailwing, and the volplane.&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;Note: Maneuverable parachutes with a glide ratio L/D of 2.5 or better have been defined in the literature as &amp;quot;hi-glide parachutes.&amp;quot; This includes the parawing, the parafoil, the sailwing, and the volplane.&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:TABLE 5-5. Ballon-Type Decelerators..jpg|center|thumb|642x642px|TABLE 5-5. Ballon-Type Decelerators.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:TABLE 5-5. Ballon-Type Decelerators..jpg|center|thumb|642x642px|TABLE 5-5. Ballon-Type Decelerators.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-1. Twenty-Eight-Foot-Diameter Circular, Flat Personnel Parachute..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;456x456px&lt;/del&gt;|FIGURE 5-1. Twenty-Eight-Foot-Diameter Circular, Flat Personnel Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-1. Twenty-Eight-Foot-Diameter Circular, Flat Personnel Parachute.&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;2&lt;/ins&gt;.jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;582x582px&lt;/ins&gt;|FIGURE 5-1. Twenty-Eight-Foot-Diameter Circular, Flat Personnel Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-2. Two-Hundred-Foot-Diameter Circular, Flat Cargo Parachute..jpg|center|thumb|&lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;370x370px&lt;/del&gt;|FIGURE 5-2. Two-Hundred-Foot-Diameter Circular, Flat Cargo Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-2. Two-Hundred-Foot-Diameter Circular, Flat Cargo Parachute.&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;2&lt;/ins&gt;.jpg|center|thumb|&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;524x524px&lt;/ins&gt;|FIGURE 5-2. Two-Hundred-Foot-Diameter Circular, Flat Cargo Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-3. Army Paratrooper 35-Foot-Diameter Extended-Skirt Parachute..jpg|center|thumb|404x404px|FIGURE 5-3. Army Paratrooper 35-Foot-Diameter Extended-Skirt Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-3. Army Paratrooper 35-Foot-Diameter Extended-Skirt Parachute..jpg|center|thumb|404x404px|FIGURE 5-3. Army Paratrooper 35-Foot-Diameter Extended-Skirt Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-4. Twenty-Four-Foot-Diameter Hemispherical Parachute..jpg|center|thumb|405x405px|FIGURE 5-4. Twenty-Four-Foot-Diameter Hemispherical Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;[[File:FIGURE 5-4. Twenty-Four-Foot-Diameter Hemispherical Parachute..jpg|center|thumb|405x405px|FIGURE 5-4. Twenty-Four-Foot-Diameter Hemispherical Parachute.]]&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/table&gt;</summary>
		<author><name>Parachute</name></author>
	</entry>
	<entry>
		<id>https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=716&amp;oldid=prev</id>
		<title>Parachute at 22:47, 25 June 2024</title>
		<link rel="alternate" type="text/html" href="https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=716&amp;oldid=prev"/>
		<updated>2024-06-25T22:47:18Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;table style=&quot;background-color: #fff; color: #202122;&quot; data-mw=&quot;interface&quot;&gt;
				&lt;col class=&quot;diff-marker&quot; /&gt;
				&lt;col class=&quot;diff-content&quot; /&gt;
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				&lt;col class=&quot;diff-content&quot; /&gt;
				&lt;tr class=&quot;diff-title&quot; lang=&quot;en&quot;&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;← Older revision&lt;/td&gt;
				&lt;td colspan=&quot;2&quot; style=&quot;background-color: #fff; color: #202122; text-align: center;&quot;&gt;Revision as of 22:47, 25 June 2024&lt;/td&gt;
				&lt;/tr&gt;&lt;tr&gt;&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot; id=&quot;mw-diff-left-l1508&quot;&gt;Line 1,508:&lt;/td&gt;
&lt;td colspan=&quot;2&quot; class=&quot;diff-lineno&quot;&gt;Line 1,508:&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.164. W D. Brown. Parachutes. Pub. by Sir Isaac Pitman &amp;amp; Sons, LTD, London, July 1948.&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.164. W D. Brown. Parachutes. Pub. by Sir Isaac Pitman &amp;amp; Sons, LTD, London, July 1948.&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;−&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.165. B. K. Baca. 'An Experimental Study of the Performance of Clustered Parachutes in a Low Speed Wind &lt;del style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;l'nnel&lt;/del&gt;.&quot; AIAA Paper, April 1984. (AIAA 84-0822.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot; data-marker=&quot;+&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.165. B. K. Baca. 'An Experimental Study of the Performance of Clustered Parachutes in a Low&lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;-&lt;/ins&gt;Speed Wind &lt;ins style=&quot;font-weight: bold; text-decoration: none;&quot;&gt;Tunnel&lt;/ins&gt;.&quot; AIAA Paper, April 1984. (AIAA 84-0822.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;br&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;tr&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.166. U.S. Air Force. Extraction Parachute Clustering Techniques, by C. W Marshall. USAF, October 1958. (USAF Report FTC-TN-58-18.)&lt;/div&gt;&lt;/td&gt;&lt;td class=&quot;diff-marker&quot;&gt;&lt;/td&gt;&lt;td style=&quot;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;&quot;&gt;&lt;div&gt;5.166. U.S. Air Force. Extraction Parachute Clustering Techniques, by C. W Marshall. USAF, October 1958. (USAF Report FTC-TN-58-18.)&lt;/div&gt;&lt;/td&gt;&lt;/tr&gt;
&lt;/table&gt;</summary>
		<author><name>Parachute</name></author>
	</entry>
	<entry>
		<id>https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=715&amp;oldid=prev</id>
		<title>Parachute at 20:48, 25 June 2024</title>
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		<updated>2024-06-25T20:48:12Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
&lt;a href=&quot;https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;amp;diff=715&amp;amp;oldid=714&quot;&gt;Show changes&lt;/a&gt;</summary>
		<author><name>Parachute</name></author>
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	<entry>
		<id>https://mediawiki.aerodecelerator.org/index.php?title=Parachute_Performance&amp;diff=714&amp;oldid=prev</id>
		<title>Parachute at 20:42, 25 June 2024</title>
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		<updated>2024-06-25T20:42:48Z</updated>

		<summary type="html">&lt;p&gt;&lt;/p&gt;
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		<author><name>Parachute</name></author>
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