Survivability considerations during aircraft conceptual design
dc.contributor.advisor | Ball, R.E. | |
dc.contributor.author | Gilman, Robert John | |
dc.date | March 1986 | |
dc.date.accessioned | 2012-11-27T00:18:25Z | |
dc.date.available | 2012-11-27T00:18:25Z | |
dc.date.issued | 1986-03 | |
dc.identifier.uri | https://hdl.handle.net/10945/22138 | |
dc.description.abstract | Survivability, capability, maintainability, and reliability will establish the effectiveness of a combat aircraft. Considerations for the "ilities" must take place during the conceptual design phase. Retrofit of survivability enhancement has historically increased weight, drag, and cost, while decreasing capability and performance. Proper application of the six susceptibility reduction concepts and the six vulnerability reduction concepts must take place before the design is established to maximize effectiveness and minimize penalties. In this thesis, the application of survivability enhancement techniques to the conceptual design is presented in general and also specifically applied to the design of a long range Strike Fighter aircraft. General guidelines for susceptibility and vulnerability reduction for any aircraft are also presented. | |
dc.description.uri | http://archive.org/details/survivabilitycon1094522138 | |
dc.format.extent | 99 p. | en_US |
dc.language.iso | en_US | |
dc.rights | This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States. | |
dc.subject.lcsh | Aeronautics | en_US |
dc.title | Survivability considerations during aircraft conceptual design | en_US |
dc.type | Thesis | en_US |
dc.contributor.corporate | Naval Postgraduate School (U.S.) | |
dc.contributor.department | Aeronautics | |
dc.subject.author | Aircraft survivability | en_US |
dc.subject.author | Susceptability | en_US |
dc.subject.author | Vulnerability | en_US |
dc.subject.author | Conceptual design | en_US |
dc.description.service | Lieutenant, United States Navy | |
etd.thesisdegree.name | M.S. in Aeronautical Engineering | en_US |
etd.thesisdegree.level | Masters | en_US |
etd.thesisdegree.discipline | Aeronautical Engineering | en_US |
etd.thesisdegree.grantor | Naval Postgraduate School | en_US |
dc.description.distributionstatement | Approved for public release; distribution is unlimited. |
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