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F-15 propulsion systemA brief description of the NASA F-15 research aircraft propulsion system is given. The F-15 is powered by two PW1128 afterburning turbofan engines which are growth versions of the F100-PW-100 engine. The PW1128 is controlled by a full-authority digital electronic engine control (DEEC). The F-15 inlet is a two-dimensional, three-ramp, external compression design with partially cut back side plates. Each inlet is independently controlled by an electronic air inlet controller (EAIC).
Document ID
19950026591
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bushman, Mark (Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Nobbs, Steven G. (McDonnell-Douglas Corp. Saint Louis, MO., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publication: NASA. Dryden Flight Research Center, An Electronic Workshop on the Performance Seeking Control and Propulsion Controlled Aircraft Results of the F-15 Highly Integrated Digital Electronic Control Flight Research Program
Subject Category
Aircraft Propulsion And Power
Accession Number
95N33012
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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