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dc.contributor.advisorWesley L. Harris and Daniel E. Hastings.en_US
dc.contributor.authorLewis, Spencer L. (Spencer Lawrence), 1975-en_US
dc.contributor.otherManagement of Technology Program.en_US
dc.date.accessioned2005-08-22T23:52:24Z
dc.date.available2005-08-22T23:52:24Z
dc.date.copyright2000en_US
dc.date.issued2000en_US
dc.identifier.urihttp://theses.mit.edu/Dienst/UI/2.0/Describe/0018.mit.theses%2f2000-117en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/9256
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics; and, (S.M.)--Massachusetts Institute of Technology, Technology and Policy Program, 2000.en_US
dc.descriptionAlso available online at the MIT Theses Online homepage <http://thesis.mit.edu>.en_US
dc.descriptionIncludes bibliographical references (p. 99-101).en_US
dc.description.abstractThe United States Air Force utilizes a significant amount of its budget to maintain its aerospace systems in operational condition. In order to reduce these costs, the Air Force has communicated to aerospace manufactures a desire to reduce the overall costs of its aerospace system maintenance. This thesis investigates how the Air Force and Corporation Alpha, a leading manufacturer of aerospace engines, have adapted their design and development practices to make the EG10 fighter engine family more reliable, durable, and maintainable. I used the metric Unscheduled Engine Removals (UER) per 1000 Effective Flight Hours (UER/1000EFH) to compare the sustainability of different models of EG10 while investigating how the sustainment lessons of the EG10 have been incorporated into Corporation Alpha's latest product, the EG1 5-1. The analysis presented in this thesis will focus on the policies, technology, processes and tools, and final results of efforts to improve the sustainability of these engine systems. The final results show that the sustainability, as measured by the UER metric, have not increased beyond 106 EFH with each succeeding generation of EG10 engine. This illustrates that improving aerospace system sustainability involves factors beyond the design phase of the system.en_US
dc.description.statementofresponsibilityby Spencer L. Lewis.en_US
dc.format.extent106 p.en_US
dc.format.extent7165766 bytes
dc.format.extent7165528 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://theses.mit.edu/Dienst/UI/2.0/Describe/0018.mit.theses%2f2000-117en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582
dc.subjectAeronautics and Astronautics.en_US
dc.subjectManagement of Technology Program.en_US
dc.titleDesigning for sustainability & upgradability in an aerospace systemen_US
dc.title.alternativeDesigning for sustainability and upgradeability in an aerospace systemen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentManagement of Technology Program.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.contributor.departmentTechnology and Policy Program
dc.identifier.oclc45537523en_US


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