NASA NTRS · 19950026591
F-15 propulsion system
Abstract
A 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).
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Bushman, Mark, Nobbs, Steven G.. 1995-01-01. F-15 propulsion system. https://ntrs.nasa.gov/citations/19950026591
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