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SAE AIR 5642:2005-06-07

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SAE AIR 5642:2005-06-07

The Effect of Installation Power Losses on the Overall Performance of a Helicopter

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The purpose of this SAE Aerospace Information Report (AIR) is to illustrate the effect of installation power losses on the performance of a helicopter. Installation power losses result from a variety of sources, some associated directly with the basic engine installation, and some coming from the installation of specific items of aircraft mission specific equipment. Close attention must be paid to the accurate measurement of these losses so that the correct aircraft performance is calculated.
Author SAE
Editor SAE
Document type Standard
Format File
ICS 49.020 : Aircraft and space vehicles in
Number of pages 17
Set AEROPAKS10U-10
Year 2005
Document history
Country USA
Keyword SAE 5642;SAE AIR5642;SAE AIR5642;SAE AIR 5642