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Preliminary flight test results of the F100 EMD engine in an F-15 airplaneA flight evaluation of the F100 Engine Model Derivative (EMD) is conducted. The F100 EMD is an advanced version of the F100 engine that powers the F15 and F16 airplanes. The F100 EMD features a bigger fan, higher temperature turbine, a Digital Electronic Engine Control system (DEEC), and a newly designed 16 segment afterburner, all of which results in a 15 to 20 percent increase in sea level thrust. The flight evaluations consist of investigation of performance (thrust, fuel flow, and airflow) and operability (transient response and airstart) in the F-15 airplane. The performance of the F100 EMD is excellent. Aircraft acceleration time to Mach 2.0 is reduced by 23 percent with two F100 EMD engines. Several anomalies are discovered in the operability evaluations. A software change to the DEEC improved the throttle, and subsequent Cooper Harper ratings of 3 to 4 are obtained. In the extreme upper left hand corner of the flight enveloped, compressor stalls occurr when the throttle is retarded to idle power. These stalls are not predicted by altitude facility tests or stability for the compressor.
Document ID
19840016520
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Myers, L. P.
(NASA Ames Research Center Moffett Field, CA, United States)
Burcham, F. W., Jr.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-85902
NAS 1.15:85902
H-1247
Report Number: NASA-TM-85902
Report Number: NAS 1.15:85902
Report Number: H-1247
Meeting Information
Meeting: AIAA/ASME/SAE Joint Propulsion Conf.
Location: Cincinnati, OH
Country: United States
Start Date: June 11, 1984
End Date: June 13, 1984
Accession Number
84N24588
Funding Number(s)
PROJECT: RTOP 533-02-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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