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- W765973792 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)." @default.
- W765973792 created "2016-06-24" @default.
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- W765973792 date "1995-01-01" @default.
- W765973792 modified "2023-09-27" @default.
- W765973792 title "F-15 propulsion system" @default.
- W765973792 hasPublicationYear "1995" @default.
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