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Helicopter mission optimization studyThe feasibility of using low-cost, portable computer technology to help a helicopter pilot optimize flight parameters to minimize fuel consumption and takeoff and landing noise was demonstrated. Eight separate computer programs were developed for use in the helicopter cockpit using a hand-held computer. The programs provide the helicopter pilot with the ability to calculate power required, minimum fuel consumption for both range and endurance, maximum speed and a minimum noise profile for both takeoff and landing. Each program is defined by a maximum of two magnetic cards. The helicopter pilot is required to key in the proper input parameter such as gross weight, outside air temperature or pressure altitude.
Document ID
19790004865
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Olson, J. R.
(United Technologies Corp. Stratford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1978
Subject Category
Aircraft Instrumentation
Report/Patent Number
NASA-CR-3060
Report Number: NASA-CR-3060
Accession Number
79N13036
Funding Number(s)
PROJECT: RTOP 505-10-23-11
CONTRACT_GRANT: NAS1-1498
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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