Helicopter mission optimization study. Final report
Technical Report
·
OSTI ID:5912809
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.
- Research Organization:
- United Technologies Corp., Stratford, CT (USA). Sikorsky Aircraft Div.
- OSTI ID:
- 5912809
- Report Number(s):
- N-79-13036
- Country of Publication:
- United States
- Language:
- English
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