Aerothermodynamic heating and performance analysis of a high-lift aeromaneuvering AOTV concept
The thermal-control requirements for design-optimized aeromaneuvering performance are determined for space-based applications and low Earth orbit sorties involving large, multiple plane-inclination changes. The predicted aerothermodynamic heating characteristics are correlated with thermal-control a...
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| Veröffentlicht in: | Journal of spacecraft and rockets 1987-05, Vol.24 (3), p.198-204 |
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| container_end_page | 204 |
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| container_issue | 3 |
| container_start_page | 198 |
| container_title | Journal of spacecraft and rockets |
| container_volume | 24 |
| creator | Menees, Gene P Brown, Kevin G Wilson, John F Davies, Carol B |
| description | The thermal-control requirements for design-optimized aeromaneuvering performance are determined for space-based applications and low Earth orbit sorties involving large, multiple plane-inclination changes. The predicted aerothermodynamic heating characteristics are correlated with thermal-control and flight-performance capabilities. The mission payload capability for delivery, retrieval, and combined operations is determined for round-trip sorties extending to polar orbits. Recommendations are given for future design refinements. |
| doi_str_mv | 10.2514/3.25899 |
| format | Article |
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The predicted aerothermodynamic heating characteristics are correlated with thermal-control and flight-performance capabilities. The mission payload capability for delivery, retrieval, and combined operations is determined for round-trip sorties extending to polar orbits. Recommendations are given for future design refinements.</description><identifier>ISSN: 0022-4650</identifier><identifier>EISSN: 1533-6794</identifier><identifier>DOI: 10.2514/3.25899</identifier><language>eng</language><publisher>Legacy CDMS: American Institute of Aeronautics and Astronautics</publisher><subject>aerodynamics ; Aeromaneuvering ; drag ; heating ; High lift ; hypersonic flow ; Launch Vehicles And Space Vehicles ; spacecraft ; viscous flow</subject><ispartof>Journal of spacecraft and rockets, 1987-05, Vol.24 (3), p.198-204</ispartof><rights>Copyright American Institute of Aeronautics and Astronautics May/Jun 1987</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-a429t-6d5268c0d3c625311ebe6ddf70c3f8cf010d6169c2f569ab75f3d50790d0dfab3</citedby><cites>FETCH-LOGICAL-a429t-6d5268c0d3c625311ebe6ddf70c3f8cf010d6169c2f569ab75f3d50790d0dfab3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>315,781,785,27926,27927</link.rule.ids></links><search><creatorcontrib>Menees, Gene P</creatorcontrib><creatorcontrib>Brown, Kevin G</creatorcontrib><creatorcontrib>Wilson, John F</creatorcontrib><creatorcontrib>Davies, Carol B</creatorcontrib><title>Aerothermodynamic heating and performance analysis of a high-lift aeromaneuvering AOTV concept</title><title>Journal of spacecraft and rockets</title><description>The thermal-control requirements for design-optimized aeromaneuvering performance are determined for space-based applications and low Earth orbit sorties involving large, multiple plane-inclination changes. 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Recommendations are given for future design refinements.</description><subject>aerodynamics</subject><subject>Aeromaneuvering</subject><subject>drag</subject><subject>heating</subject><subject>High lift</subject><subject>hypersonic flow</subject><subject>Launch Vehicles And Space Vehicles</subject><subject>spacecraft</subject><subject>viscous flow</subject><issn>0022-4650</issn><issn>1533-6794</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1987</creationdate><recordtype>article</recordtype><sourceid>CYI</sourceid><recordid>eNqN0UtrFTEUAOAgCl6r-AdcDFgsXYw9eU6yvBT7gEI3tUtDbh69U2Ym0yQj3n9v6i0UioirQzjfeZCD0EcMXwnH7ITWIJV6hVaYU9qKTrHXaAVASMsEh7foXc73AFhIoVbox9qnWLY-jdHtJjP2ttl6U_rprjGTa2afQkyjmayvbzPscp-bGBrTbPu7bTv0oTSmdqjCLz99eqxbX9_cNjbWkrm8R2-CGbL_8BQP0PezbzenF-3V9fnl6fqqNYyo0grHiZAWHLWCcIqx33jhXOjA0iBtAAxOYKEsCVwos-l4oI5Dp8CBC2ZDD9DRvu-c4sPic9Fjn60fhrpXXLLuGFMSuMJVfvmnJEwIqZj6T0igws8v4H1cUv2sarDAHRNSds8b2hRzTj7oOfWjSTuNQT8eTlP953BVftrLyWSjp5Kyxkp2AJxRImv6eJ82vTHPo56q9eyCDsswFP-rVHv4N_ty4m8vx6xt</recordid><startdate>19870501</startdate><enddate>19870501</enddate><creator>Menees, Gene P</creator><creator>Brown, Kevin G</creator><creator>Wilson, John F</creator><creator>Davies, Carol B</creator><general>American Institute of Aeronautics and Astronautics</general><scope>CYE</scope><scope>CYI</scope><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>19870501</creationdate><title>Aerothermodynamic heating and performance analysis of a high-lift aeromaneuvering AOTV concept</title><author>Menees, Gene P ; Brown, Kevin G ; Wilson, John F ; Davies, Carol B</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a429t-6d5268c0d3c625311ebe6ddf70c3f8cf010d6169c2f569ab75f3d50790d0dfab3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1987</creationdate><topic>aerodynamics</topic><topic>Aeromaneuvering</topic><topic>drag</topic><topic>heating</topic><topic>High lift</topic><topic>hypersonic flow</topic><topic>Launch Vehicles And Space Vehicles</topic><topic>spacecraft</topic><topic>viscous flow</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Menees, Gene P</creatorcontrib><creatorcontrib>Brown, Kevin G</creatorcontrib><creatorcontrib>Wilson, John F</creatorcontrib><creatorcontrib>Davies, Carol B</creatorcontrib><collection>NASA Scientific and Technical Information</collection><collection>NASA Technical Reports Server</collection><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>Menees, Gene P</au><au>Brown, Kevin G</au><au>Wilson, John F</au><au>Davies, Carol B</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Aerothermodynamic heating and performance analysis of a high-lift aeromaneuvering AOTV concept</atitle><jtitle>Journal of spacecraft and rockets</jtitle><date>1987-05-01</date><risdate>1987</risdate><volume>24</volume><issue>3</issue><spage>198</spage><epage>204</epage><pages>198-204</pages><issn>0022-4650</issn><eissn>1533-6794</eissn><abstract>The thermal-control requirements for design-optimized aeromaneuvering performance are determined for space-based applications and low Earth orbit sorties involving large, multiple plane-inclination changes. The predicted aerothermodynamic heating characteristics are correlated with thermal-control and flight-performance capabilities. The mission payload capability for delivery, retrieval, and combined operations is determined for round-trip sorties extending to polar orbits. Recommendations are given for future design refinements.</abstract><cop>Legacy CDMS</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/3.25899</doi><tpages>7</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0022-4650 |
| ispartof | Journal of spacecraft and rockets, 1987-05, Vol.24 (3), p.198-204 |
| issn | 0022-4650 1533-6794 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_24668920 |
| source | NASA Technical Reports Server; Alma/SFX Local Collection |
| subjects | aerodynamics Aeromaneuvering drag heating High lift hypersonic flow Launch Vehicles And Space Vehicles spacecraft viscous flow |
| title | Aerothermodynamic heating and performance analysis of a high-lift aeromaneuvering AOTV concept |
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