A new rotating parachute design having high performance
A new concept of rotating parachute has been designed primarily for recovery of high-performance re-entry vehicles. Design and development/testing results are presented from low-speed wind tunnel testing, free-flight deployments at transonic speeds, and tests in a supersonic wind tunnel at Mach 2.0....
Gespeichert in:
| Veröffentlicht in: | Journal of spacecraft and rockets 1986-03, Vol.23 (2), p.222-224 |
|---|---|
| 1. Verfasser: | |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 224 |
|---|---|
| container_issue | 2 |
| container_start_page | 222 |
| container_title | Journal of spacecraft and rockets |
| container_volume | 23 |
| creator | Pepper, William B |
| description | A new concept of rotating parachute has been designed primarily for recovery of high-performance re-entry vehicles. Design and development/testing results are presented from low-speed wind tunnel testing, free-flight deployments at transonic speeds, and tests in a supersonic wind tunnel at Mach 2.0. Drag coefficients of 1.25 based on the disk area of the 2-ft-diam rotor have been measured in the wind tunnel. The stability of the rotor is excellent, with oscillation of its centerline being less than 3 deg. Good agreement between theoretical and measured performance parameters is shown. |
| doi_str_mv | 10.2514/3.25102 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_crossref_primary_10_2514_3_25102</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>24176654</sourcerecordid><originalsourceid>FETCH-LOGICAL-a408t-392ea9476fba927518eb9650f02461491a7867457abaae59103ae85f987b31693</originalsourceid><addsrcrecordid>eNqN0VlLw0AQAOBFFKxV_AsBRfEhuvfxKMULCr7o8zJJd5uUNIm7ice_N7WFgor4NDDzMcyB0DHBl1QQfsVWAdMdNCKCsVQqw3fRCGNKUy4F3kcHMS4wJlJLM0LqOqndWxKaDrqynictBMiLvnPJzMVyXicFvK7yRTkvktYF34Ql1Lk7RHsequiONnGMnm9vnib36fTx7mFyPU2BY92lzFAHhivpMzBUCaJdZoYpPKZcEm4IKC0VFwoyACcMwQycFt5olTEiDRuj83XfNjQvvYudXZYxd1UFtWv6aBXnRmHD9SDP_pSUEyWl4P-CwwXZAE--wUXTh3pY11IiiWJGSb2dMA9NjMF524ZyCeHDEmxXH7HMfn1kkKdrCSXAttdPdvEb25RtO_PW91XVufeOfQJYI5Ny</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2161739768</pqid></control><display><type>article</type><title>A new rotating parachute design having high performance</title><source>Alma/SFX Local Collection</source><creator>Pepper, William B</creator><creatorcontrib>Pepper, William B</creatorcontrib><description>A new concept of rotating parachute has been designed primarily for recovery of high-performance re-entry vehicles. Design and development/testing results are presented from low-speed wind tunnel testing, free-flight deployments at transonic speeds, and tests in a supersonic wind tunnel at Mach 2.0. Drag coefficients of 1.25 based on the disk area of the 2-ft-diam rotor have been measured in the wind tunnel. The stability of the rotor is excellent, with oscillation of its centerline being less than 3 deg. Good agreement between theoretical and measured performance parameters is shown.</description><identifier>ISSN: 0022-4650</identifier><identifier>EISSN: 1533-6794</identifier><identifier>DOI: 10.2514/3.25102</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>aerodynamics ; drag ; Parachutes ; space vehicles ; wind tunnels</subject><ispartof>Journal of spacecraft and rockets, 1986-03, Vol.23 (2), p.222-224</ispartof><rights>Copyright American Institute of Aeronautics and Astronautics Mar/Apr 1986</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a408t-392ea9476fba927518eb9650f02461491a7867457abaae59103ae85f987b31693</citedby><cites>FETCH-LOGICAL-a408t-392ea9476fba927518eb9650f02461491a7867457abaae59103ae85f987b31693</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Pepper, William B</creatorcontrib><title>A new rotating parachute design having high performance</title><title>Journal of spacecraft and rockets</title><description>A new concept of rotating parachute has been designed primarily for recovery of high-performance re-entry vehicles. Design and development/testing results are presented from low-speed wind tunnel testing, free-flight deployments at transonic speeds, and tests in a supersonic wind tunnel at Mach 2.0. Drag coefficients of 1.25 based on the disk area of the 2-ft-diam rotor have been measured in the wind tunnel. The stability of the rotor is excellent, with oscillation of its centerline being less than 3 deg. Good agreement between theoretical and measured performance parameters is shown.</description><subject>aerodynamics</subject><subject>drag</subject><subject>Parachutes</subject><subject>space vehicles</subject><subject>wind tunnels</subject><issn>0022-4650</issn><issn>1533-6794</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1986</creationdate><recordtype>article</recordtype><recordid>eNqN0VlLw0AQAOBFFKxV_AsBRfEhuvfxKMULCr7o8zJJd5uUNIm7ice_N7WFgor4NDDzMcyB0DHBl1QQfsVWAdMdNCKCsVQqw3fRCGNKUy4F3kcHMS4wJlJLM0LqOqndWxKaDrqynictBMiLvnPJzMVyXicFvK7yRTkvktYF34Ql1Lk7RHsequiONnGMnm9vnib36fTx7mFyPU2BY92lzFAHhivpMzBUCaJdZoYpPKZcEm4IKC0VFwoyACcMwQycFt5olTEiDRuj83XfNjQvvYudXZYxd1UFtWv6aBXnRmHD9SDP_pSUEyWl4P-CwwXZAE--wUXTh3pY11IiiWJGSb2dMA9NjMF524ZyCeHDEmxXH7HMfn1kkKdrCSXAttdPdvEb25RtO_PW91XVufeOfQJYI5Ny</recordid><startdate>19860301</startdate><enddate>19860301</enddate><creator>Pepper, William B</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><scope>7TC</scope></search><sort><creationdate>19860301</creationdate><title>A new rotating parachute design having high performance</title><author>Pepper, William B</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a408t-392ea9476fba927518eb9650f02461491a7867457abaae59103ae85f987b31693</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1986</creationdate><topic>aerodynamics</topic><topic>drag</topic><topic>Parachutes</topic><topic>space vehicles</topic><topic>wind tunnels</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Pepper, William B</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Mechanical Engineering Abstracts</collection><jtitle>Journal of spacecraft and rockets</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Pepper, William B</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>A new rotating parachute design having high performance</atitle><jtitle>Journal of spacecraft and rockets</jtitle><date>1986-03-01</date><risdate>1986</risdate><volume>23</volume><issue>2</issue><spage>222</spage><epage>224</epage><pages>222-224</pages><issn>0022-4650</issn><eissn>1533-6794</eissn><abstract>A new concept of rotating parachute has been designed primarily for recovery of high-performance re-entry vehicles. Design and development/testing results are presented from low-speed wind tunnel testing, free-flight deployments at transonic speeds, and tests in a supersonic wind tunnel at Mach 2.0. Drag coefficients of 1.25 based on the disk area of the 2-ft-diam rotor have been measured in the wind tunnel. The stability of the rotor is excellent, with oscillation of its centerline being less than 3 deg. Good agreement between theoretical and measured performance parameters is shown.</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/3.25102</doi><tpages>3</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0022-4650 |
| ispartof | Journal of spacecraft and rockets, 1986-03, Vol.23 (2), p.222-224 |
| issn | 0022-4650 1533-6794 |
| language | eng |
| recordid | cdi_crossref_primary_10_2514_3_25102 |
| source | Alma/SFX Local Collection |
| subjects | aerodynamics drag Parachutes space vehicles wind tunnels |
| title | A new rotating parachute design having high performance |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-08T08%3A31%3A16IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=A%20new%20rotating%20parachute%20design%20having%20high%20performance&rft.jtitle=Journal%20of%20spacecraft%20and%20rockets&rft.au=Pepper,%20William%20B&rft.date=1986-03-01&rft.volume=23&rft.issue=2&rft.spage=222&rft.epage=224&rft.pages=222-224&rft.issn=0022-4650&rft.eissn=1533-6794&rft_id=info:doi/10.2514/3.25102&rft_dat=%3Cproquest_cross%3E24176654%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2161739768&rft_id=info:pmid/&rfr_iscdi=true |