Aircrew centered system design analysis considerations for the MH-53E helicopter

Aircrew centered system design analysis considerations for the MH-53E helicopter

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Approved for public release; distribution is unlimited === An analysis was made of the aircrew centered system design aspects for the MH-53E helicopter. These aircrew centered design features included changes in the cockpit, aircraft weight, and drag coefficient. The cockpit evaluation compared the...

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Main Author: Gibson, Gregory J.
Other Authors: Newberry, Conrad F.
Language:en_US
Published: Monterey, California. Naval Postgraduate School 2012
Online Access:http://hdl.handle.net/10945/7862
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spelling ndltd-nps.edu-oai-calhoun.nps.edu-10945-78622015-06-20T16:02:33Z Aircrew centered system design analysis considerations for the MH-53E helicopter Gibson, Gregory J. Newberry, Conrad F. Wood, E. Roberts Naval Postgraduate School Department of Aeronautical Engineering Approved for public release; distribution is unlimited An analysis was made of the aircrew centered system design aspects for the MH-53E helicopter. These aircrew centered design features included changes in the cockpit, aircraft weight, and drag coefficient. The cockpit evaluation compared the current MH-53E cockpit configuration with design changes currently under review by the Navy. This evaluation suggests that the proposed cockpit design display change may reduce aircrew load stress and improve mission effectiveness. Changes in subsystem components may either increase or decrease the weight of the MH-53E. Similarly, changes in crew tasking may result in a need for more or less fuselage volume size. Therefore, the sensitivity of MH-53E performance to generic changes in weight and drag was investigated in order to make source assessment of equipment and crew tasking changes upon MH-53E mission effectiveness 2012-08-09T19:16:56Z 2012-08-09T19:16:56Z 1996-12 Thesis http://hdl.handle.net/10945/7862 en_US This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, it may not be copyrighted. Monterey, California. Naval Postgraduate School
collection NDLTD
language en_US
sources NDLTD
description Approved for public release; distribution is unlimited === An analysis was made of the aircrew centered system design aspects for the MH-53E helicopter. These aircrew centered design features included changes in the cockpit, aircraft weight, and drag coefficient. The cockpit evaluation compared the current MH-53E cockpit configuration with design changes currently under review by the Navy. This evaluation suggests that the proposed cockpit design display change may reduce aircrew load stress and improve mission effectiveness. Changes in subsystem components may either increase or decrease the weight of the MH-53E. Similarly, changes in crew tasking may result in a need for more or less fuselage volume size. Therefore, the sensitivity of MH-53E performance to generic changes in weight and drag was investigated in order to make source assessment of equipment and crew tasking changes upon MH-53E mission effectiveness
author2 Newberry, Conrad F.
author_facet Newberry, Conrad F.
Gibson, Gregory J.
author Gibson, Gregory J.
spellingShingle Gibson, Gregory J.
Aircrew centered system design analysis considerations for the MH-53E helicopter
author_sort Gibson, Gregory J.
title Aircrew centered system design analysis considerations for the MH-53E helicopter
title_short Aircrew centered system design analysis considerations for the MH-53E helicopter
title_full Aircrew centered system design analysis considerations for the MH-53E helicopter
title_fullStr Aircrew centered system design analysis considerations for the MH-53E helicopter
title_full_unstemmed Aircrew centered system design analysis considerations for the MH-53E helicopter
title_sort aircrew centered system design analysis considerations for the mh-53e helicopter
publisher Monterey, California. Naval Postgraduate School
publishDate 2012
url http://hdl.handle.net/10945/7862
work_keys_str_mv AT gibsongregoryj aircrewcenteredsystemdesignanalysisconsiderationsforthemh53ehelicopter
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