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AERODYNAMIC CHARACTERISTICS OF VARIOUS TYPES OF FULL SCALE PARACHUTES AT MACH NUMBERS FROM 1.8 TO 3.0
As an extension of studies previously completed in the von Karman Gas Dynamics Facility, a test was conducted in the Propulsion Wind Tunnel, Supersonic (16S), to determine the effect of Mach number on the drag, stability, and inflation characteristics of four types of parachutes. The parachute chara...
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creator | Lowry, J F |
description | As an extension of studies previously completed in the von Karman Gas Dynamics Facility, a test was conducted in the Propulsion Wind Tunnel, Supersonic (16S), to determine the effect of Mach number on the drag, stability, and inflation characteristics of four types of parachutes. The parachute characteristics were investigated at Mach numbers from 1.8 to 3.0 at pressure altitudes from 75,000 to 104,000 ft. Hyperflo parachutes were tested with 14 different roof configurations, hemisflo and conical parachutes with two different shroud line lengths and a butted skirt. A supersonic-guide-surface parachute was tested at various parachute-centerbody separation distances. |
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The parachute characteristics were investigated at Mach numbers from 1.8 to 3.0 at pressure altitudes from 75,000 to 104,000 ft. Hyperflo parachutes were tested with 14 different roof configurations, hemisflo and conical parachutes with two different shroud line lengths and a butted skirt. A supersonic-guide-surface parachute was tested at various parachute-centerbody separation distances.</description><language>eng</language><subject>DECELERATION ; DEPLOYMENT ; DROGUE PARACHUTES ; Gliders and Parachutes ; GUIDED MISSILES ; HEMISFLO PARACHUTES ; HIGH ALTITUDE ; HYPERFLO PARACHUTES ; MODEL TESTS ; PARACHUTES ; PERFORMANCE(ENGINEERING) ; POROSITY ; RIBBON PARACHUTES ; SIMULATION ; SUPERSONIC CHARACTERISTICS ; WIND TUNNEL MODELS</subject><creationdate>1964</creationdate><rights>Approved for public release; distribution is unlimited.</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27567,27568</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0351001$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Lowry, J F</creatorcontrib><creatorcontrib>ARO INC ARNOLD AFS TN</creatorcontrib><title>AERODYNAMIC CHARACTERISTICS OF VARIOUS TYPES OF FULL SCALE PARACHUTES AT MACH NUMBERS FROM 1.8 TO 3.0</title><description>As an extension of studies previously completed in the von Karman Gas Dynamics Facility, a test was conducted in the Propulsion Wind Tunnel, Supersonic (16S), to determine the effect of Mach number on the drag, stability, and inflation characteristics of four types of parachutes. The parachute characteristics were investigated at Mach numbers from 1.8 to 3.0 at pressure altitudes from 75,000 to 104,000 ft. Hyperflo parachutes were tested with 14 different roof configurations, hemisflo and conical parachutes with two different shroud line lengths and a butted skirt. A supersonic-guide-surface parachute was tested at various parachute-centerbody separation distances.</description><subject>DECELERATION</subject><subject>DEPLOYMENT</subject><subject>DROGUE PARACHUTES</subject><subject>Gliders and Parachutes</subject><subject>GUIDED MISSILES</subject><subject>HEMISFLO PARACHUTES</subject><subject>HIGH ALTITUDE</subject><subject>HYPERFLO PARACHUTES</subject><subject>MODEL TESTS</subject><subject>PARACHUTES</subject><subject>PERFORMANCE(ENGINEERING)</subject><subject>POROSITY</subject><subject>RIBBON PARACHUTES</subject><subject>SIMULATION</subject><subject>SUPERSONIC CHARACTERISTICS</subject><subject>WIND TUNNEL MODELS</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1964</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFirEKwjAURbM4iPoHDu8HLAlFcH2mCQk0TUlehE5FNEJBXJr_xyruTvdwzl2zjCr4ZujQWQnSYEBJKthIVkbwGi4YrE8RaOjVV-jUthAltgr6z9skWgISuIWhS-6sQgQdvANRnYA81BXfstXj-pzz7rcbtteKpDncy3Qb5zK9chmx4fVRcC7qP_kNNMEw3g</recordid><startdate>196406</startdate><enddate>196406</enddate><creator>Lowry, J F</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>196406</creationdate><title>AERODYNAMIC CHARACTERISTICS OF VARIOUS TYPES OF FULL SCALE PARACHUTES AT MACH NUMBERS FROM 1.8 TO 3.0</title><author>Lowry, J F</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD03510013</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1964</creationdate><topic>DECELERATION</topic><topic>DEPLOYMENT</topic><topic>DROGUE PARACHUTES</topic><topic>Gliders and Parachutes</topic><topic>GUIDED MISSILES</topic><topic>HEMISFLO PARACHUTES</topic><topic>HIGH ALTITUDE</topic><topic>HYPERFLO PARACHUTES</topic><topic>MODEL TESTS</topic><topic>PARACHUTES</topic><topic>PERFORMANCE(ENGINEERING)</topic><topic>POROSITY</topic><topic>RIBBON PARACHUTES</topic><topic>SIMULATION</topic><topic>SUPERSONIC CHARACTERISTICS</topic><topic>WIND TUNNEL MODELS</topic><toplevel>online_resources</toplevel><creatorcontrib>Lowry, J F</creatorcontrib><creatorcontrib>ARO INC ARNOLD AFS TN</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Lowry, J F</au><aucorp>ARO INC ARNOLD AFS TN</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>AERODYNAMIC CHARACTERISTICS OF VARIOUS TYPES OF FULL SCALE PARACHUTES AT MACH NUMBERS FROM 1.8 TO 3.0</btitle><date>1964-06</date><risdate>1964</risdate><abstract>As an extension of studies previously completed in the von Karman Gas Dynamics Facility, a test was conducted in the Propulsion Wind Tunnel, Supersonic (16S), to determine the effect of Mach number on the drag, stability, and inflation characteristics of four types of parachutes. The parachute characteristics were investigated at Mach numbers from 1.8 to 3.0 at pressure altitudes from 75,000 to 104,000 ft. Hyperflo parachutes were tested with 14 different roof configurations, hemisflo and conical parachutes with two different shroud line lengths and a butted skirt. A supersonic-guide-surface parachute was tested at various parachute-centerbody separation distances.</abstract><oa>free_for_read</oa></addata></record> |
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source | DTIC Technical Reports |
subjects | DECELERATION DEPLOYMENT DROGUE PARACHUTES Gliders and Parachutes GUIDED MISSILES HEMISFLO PARACHUTES HIGH ALTITUDE HYPERFLO PARACHUTES MODEL TESTS PARACHUTES PERFORMANCE(ENGINEERING) POROSITY RIBBON PARACHUTES SIMULATION SUPERSONIC CHARACTERISTICS WIND TUNNEL MODELS |
title | AERODYNAMIC CHARACTERISTICS OF VARIOUS TYPES OF FULL SCALE PARACHUTES AT MACH NUMBERS FROM 1.8 TO 3.0 |
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