Energy Efficient Engine Flight Propulsion System Preliminary Analysis and Design Report
Energy Efficient Engine Flight Propulsion System Preliminary Analysis and Design Report
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A flight propulsion system preliminary design was established that meets the program goals of at least a 12 percent reduction in thrust specific fuel consumption, at least a five percent reduction in direct operating cost, and one-half the performance deterioration rate of the most efficient current commercial engines. The engine provides a high probability of meeting the 1978 noise rule goal. Smoke and gaseous emissions defined by the EPA proposed standards for engines newly certified after 1 January 1981 are met with the exception of NOx, despite incorporation of all known NOx reduction technology.
Document information
Energy Efficient Engine Flight Propulsion System Preliminary Analysis and Design Report
1979
480 pages
Report
No indication
English