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SAE AIR 1850A:1997-06-01

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SAE AIR 1850A:1997-06-01

Twin Engine Helicopter Power Requirements

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This SAE Aerospace Information Report (AIR) defines the power spectrum during normal and emergency operations of a twin engine helicopter and thereby postulates suitable power plant rating structures. This document does not address the power requirements for single engine helicopters or those with more than two engines.
Author SAE
Editor SAE
Document type Standard
Format File
ICS 49.050 : Aerospace engines and propulsion systems
Number of pages 8
Replace SAE AIR 1850:1989-03-13
Set AEROPAKS10U-10
Year 1990
Document history SAE AIR 1850:1989-03-13
Country USA
Keyword SAE 1850;SAE AIR1850A;SAE AIR1850A;SAE AIR 1850