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Status review of NASA programs for reducing aircraft gas turbine engine emissionsPrograms initiated by NASA to develop and demonstrate low emission advanced technology combustors for reducing aircraft gas turbine engine pollution are reviewed. Program goals are consistent with urban emission level requirements as specified by the U. S. Environmental Protection Agency and with upper atmosphere cruise emission levels as recommended by the U. S. Climatic Impact Assessment Program and National Research Council. Preliminary tests of advanced technology combustors indicate that significant reductions in all major pollutant emissions should be attainable in present generation aircraft gas turbine engines without adverse effects on fuel consumption. Preliminary test results from fundamental studies indicate that extremely low emission combustion systems may be possible for future generation jet aircraft. The emission reduction techniques currently being evaluated in these programs are described along with the results and a qualitative assessment of development difficulty.
Document ID
19760008992
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rudey, R. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-8620
NASA-TM-X-71861
Meeting Information
Meeting: Intern. Symp. on Air Breathing Engines
Location: Munich
Country: Germany
Start Date: March 7, 1976
End Date: March 12, 1976
Accession Number
76N16080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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