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NASA NTRS ยท 19790004865

Helicopter mission optimization study

Abstract

The 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.

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BibTeXRIS

Olson, J. R.. 1978-12-01. Helicopter mission optimization study. https://ntrs.nasa.gov/citations/19790004865

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