Designing for sustainability & upgradability in an aerospace system

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 bibliographica...

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Main Author: Lewis, Spencer L. (Spencer Lawrence), 1975-
Other Authors: Wesley L. Harris and Daniel E. Hastings.
Format: Others
Language:English
Published: Massachusetts Institute of Technology 2005
Subjects:
Online Access:http://theses.mit.edu/Dienst/UI/2.0/Describe/0018.mit.theses%2f2000-117
http://hdl.handle.net/1721.1/9256
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spelling ndltd-MIT-oai-dspace.mit.edu-1721.1-92562019-05-02T16:33:37Z Designing for sustainability & upgradability in an aerospace system Designing for sustainability and upgradeability in an aerospace system Lewis, Spencer L. (Spencer Lawrence), 1975- Wesley L. Harris and Daniel E. Hastings. Management of Technology Program. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Management of Technology Program. Aeronautics and Astronautics. Management of Technology Program. 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). 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. by Spencer L. Lewis. S.M. 2005-08-22T23:52:24Z 2005-08-22T23:52:24Z 2000 2000 Thesis http://theses.mit.edu/Dienst/UI/2.0/Describe/0018.mit.theses%2f2000-117 http://hdl.handle.net/1721.1/9256 45537523 eng 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 106 p. 7165766 bytes 7165528 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology
collection NDLTD
language English
format Others
sources NDLTD
topic Aeronautics and Astronautics.
Management of Technology Program.
spellingShingle Aeronautics and Astronautics.
Management of Technology Program.
Lewis, Spencer L. (Spencer Lawrence), 1975-
Designing for sustainability & upgradability in an aerospace 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). === 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. === by Spencer L. Lewis. === S.M.
author2 Wesley L. Harris and Daniel E. Hastings.
author_facet Wesley L. Harris and Daniel E. Hastings.
Lewis, Spencer L. (Spencer Lawrence), 1975-
author Lewis, Spencer L. (Spencer Lawrence), 1975-
author_sort Lewis, Spencer L. (Spencer Lawrence), 1975-
title Designing for sustainability & upgradability in an aerospace system
title_short Designing for sustainability & upgradability in an aerospace system
title_full Designing for sustainability & upgradability in an aerospace system
title_fullStr Designing for sustainability & upgradability in an aerospace system
title_full_unstemmed Designing for sustainability & upgradability in an aerospace system
title_sort designing for sustainability & upgradability in an aerospace system
publisher Massachusetts Institute of Technology
publishDate 2005
url http://theses.mit.edu/Dienst/UI/2.0/Describe/0018.mit.theses%2f2000-117
http://hdl.handle.net/1721.1/9256
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