| タイトル | Helicopter mission optimization study |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790004865 |
| 著者（英） | Olson, J. R. |
| 著者所属（英） | United Technologies Corp. |
| 発行日 | 1978-12-01 |
| 言語 | eng |
| 内容記述 | 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. |
| NASA分類 | AIRCRAFT INSTRUMENTATION |
| レポートNO | 79N13036
NASA-CR-3060 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/177093 |
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