NASA NTRS · 19800013839
Design study: A 186 kW lightweight diesel aircraft engine
Abstract
The design of an aircraft engine capable of developing 186 kW shaft power at a 7620 m altitude is described. The 186 kW design takes into account expected new developments in aircraft designs resulting in a reassessment of the power requirements at the cruise mode operation. Based on the results of this analysis a three phase technology development program is projected resulting in production dates of 1985, 1992, and 2000.
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Brouwers, A. P.. 1980-04-01. Design study: A 186 kW lightweight diesel aircraft engine. https://ntrs.nasa.gov/citations/19800013839
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