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dc.contributor.advisorNewberry, Conrad F.
dc.contributor.authorGibson, Gregory J.
dc.dateDecember 1996
dc.date.accessioned2012-08-09T19:16:56Z
dc.date.available2012-08-09T19:16:56Z
dc.date.issued1996-12
dc.identifier.urihttps://hdl.handle.net/10945/7862
dc.description.abstractAn 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 effectivenessen_US
dc.description.urihttp://archive.org/details/aircrewcentereds109457862
dc.format.extentix, 130 p.en_US
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.rightsThis 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.en_US
dc.titleAircrew centered system design analysis considerations for the MH-53E helicopteren_US
dc.typeThesisen_US
dc.contributor.secondreaderWood, E. Roberts
dc.contributor.corporateNaval Postgraduate School
dc.contributor.departmentDepartment of Aeronautical Engineering
dc.subject.authorAircrewen_US
dc.subject.authorCentereden_US
dc.subject.authorSystemen_US
dc.subject.authorDesignen_US
dc.description.serviceLieutenant, United States Navyen_US
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.


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