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Advanced Technology Spark-Ignition Aircraft Piston Engine Design StudyThe advanced technology, spark ignition, aircraft piston engine design study was conducted to determine the improvements that could be made by taking advantage of technology that could reasonably be expected to be made available for an engine intended for production by January 1, 1990. Two engines were proposed to account for levels of technology considered to be moderate risk and high risk. The moderate risk technology engine is a homogeneous charge engine operating on avgas and offers a 40% improvement in transportation efficiency over present designs. The high risk technology engine, with a stratified charge combustion system using kerosene-based jet fuel, projects a 65% improvement in transportation efficiency. Technology enablement program plans are proposed herein to set a timetable for the successful integration of each item of required advanced technology into the engine design.
Document ID
19810005452
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stuckas, K. J.
(Teledyne Continental Motors Mobile, AL, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-165162
Report Number: NASA-CR-165162
Accession Number
81N13963
Funding Number(s)
CONTRACT_GRANT: NAS3-21272
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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