Title:
Development of an Integrated Parametric Environment for Conceptual Hypersonic Missile Sizing
Development of an Integrated Parametric Environment for Conceptual Hypersonic Missile Sizing
| dc.contributor.author | Ender, Tommer Rafael | en_US |
| dc.contributor.author | McClure, Erin Kathleen | en_US |
| dc.contributor.author | Mavris, Dimitri N. | en_US |
| dc.contributor.corporatename | American Institute of Aeronautics and Astronautics | |
| dc.contributor.corporatename | Georgia Institute of Technology. Aerospace Systems Design Laboratory | |
| dc.date.accessioned | 2005-05-26T14:00:48Z | |
| dc.date.available | 2005-05-26T14:00:48Z | |
| dc.date.issued | 2002-10 | en_US |
| dc.description | Presented at the 2nd AIAA ATIO Forum, Los Angeles, CA, October 1-3, 2002. | en_US |
| dc.description.abstract | This paper outlines the method by which a graduate missile design team studying at Georgia Tech?s Aerospace System Design Laboratory (ASDL) created an environment that would link design parameters to vehicle metrics for the design of a High Speed Standoff Missile. The sizing and synthesis environment parametrically links multiple physics based disciplinary analyses, so that many aspects of the design can be studied simultaneously. That environment was then used to conceptually design a missile that best met the unobtainable requirements set by the customer. The process resulted in the conceptual design of a liquid fueled ramjet cruise missile that was compatible with the Vertical Launch System. The missile cruised at Mach 5, and was capable of striking targets up to 1462 km away. | en_US |
| dc.format.extent | 967800 bytes | |
| dc.format.extent | 1905 bytes | |
| dc.format.mimetype | application/pdf | |
| dc.format.mimetype | text/plain | |
| dc.identifier.uri | http://hdl.handle.net/1853/6296 | |
| dc.language.iso | en_US | en_US |
| dc.publisher | Georgia Institute of Technology | en_US |
| dc.publisher | Georgia Institute of Technology | |
| dc.publisher.original | American Institute of Aeronautics and Astronautics (AIAA) | |
| dc.relation.ispartofseries | ASDL;AIAA-2002-5856 | en_US |
| dc.relation.ispartofseries | ASDL;AIAA-2002-5856 | |
| dc.subject | Conceptual design | en_US |
| dc.subject | Cruise missiles | en_US |
| dc.subject | Design parameters | en_US |
| dc.subject | High speed standoff missiles | en_US |
| dc.subject | HSSM | en_US |
| dc.subject | Integrated parametric environments | en_US |
| dc.subject | Integrated sizing and synthesis environment | en_US |
| dc.subject | Metrics | en_US |
| dc.subject | Sizing tools | en_US |
| dc.subject | Vertical launch systems | en_US |
| dc.title | Development of an Integrated Parametric Environment for Conceptual Hypersonic Missile Sizing | en_US |
| dc.type | Text | |
| dc.type.genre | Paper | |
| dspace.entity.type | Publication | |
| local.contributor.author | Mavris, Dimitri N. | |
| local.contributor.corporatename | Daniel Guggenheim School of Aerospace Engineering | |
| local.contributor.corporatename | Aerospace Systems Design Laboratory (ASDL) | |
| local.contributor.corporatename | College of Engineering | |
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