The purpose of this paper is to present the analytical, developmental, and test efforts used to achieve an integrated system responsive to the U.S. Army's heavy-lift helicopter (HLH) needs. A comprehensive discussion of various approaches which were examined with particular emphasis on elements unique to this aircraft are presented. The methodology used in interfacing various components in determining the final design configuration is also presented.
Heavy-Lift Helicopter Power Systems
Sae Technical Papers
National Air Transportation Meeting ; 1974
1974-02-01
Conference paper
English
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