MIT Libraries homeMIT Libraries logoDSpace@MIT

MIT
View Item 
  • DSpace@MIT Home
  • MIT Libraries
  • MIT Theses
  • Graduate Theses
  • View Item
  • DSpace@MIT Home
  • MIT Libraries
  • MIT Theses
  • Graduate Theses
  • View Item
JavaScript is disabled for your browser. Some features of this site may not work without it.

Designing for sustainability & upgradability in an aerospace system

Author(s)
Lewis, Spencer L. (Spencer Lawrence), 1975-
Thumbnail
DownloadFull printable version (7.048Mb)
Alternative title
Designing for sustainability and upgradeability in an aerospace system
Other Contributors
Management of Technology Program.
Advisor
Wesley L. Harris and Daniel E. Hastings.
Terms of use
M.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. http://theses.mit.edu/Dienst/UI/2.0/Describe/0018.mit.theses%2f2000-117 http://dspace.mit.edu/handle/1721.1/7582
Metadata
Show full item record
Abstract
The 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.
Description
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics; and, (S.M.)--Massachusetts Institute of Technology, Technology and Policy Program, 2000.
 
Also available online at the MIT Theses Online homepage <http://thesis.mit.edu>.
 
Includes bibliographical references (p. 99-101).
 
Date issued
2000
URI
http://theses.mit.edu/Dienst/UI/2.0/Describe/0018.mit.theses%2f2000-117
http://hdl.handle.net/1721.1/9256
Department
Management of Technology Program.; Massachusetts Institute of Technology. Department of Aeronautics and Astronautics; Technology and Policy Program
Publisher
Massachusetts Institute of Technology
Keywords
Aeronautics and Astronautics., Management of Technology Program.

Collections
  • Graduate Theses

Browse

All of DSpaceCommunities & CollectionsBy Issue DateAuthorsTitlesSubjectsThis CollectionBy Issue DateAuthorsTitlesSubjects

My Account

Login

Statistics

OA StatisticsStatistics by CountryStatistics by Department
MIT Libraries homeMIT Libraries logo

Find us on

Twitter Instagram YouTube

MIT Libraries navigation

SearchHours & locationsBorrow & requestResearch supportAbout us
PrivacyPermissionsAccessibility
MIT
Massachusetts Institute of Technology
Content created by the MIT Libraries, CC BY-NC unless otherwise noted. Notify us about copyright concerns.