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F-15 propulsion system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Bushman, Mark Nobbs, Steven G. |
| Copyright Year | 1995 |
| Description | 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). |
| File Size | 159670 |
| Page Count | 4 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950026591 |
| Archival Resource Key | ark:/13960/t6c29tm3d |
| Language | English |
| Publisher Date | 1995-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Electronic Control Digital Systems Turbojet Engine Control Research Aircraft Engine Inlets Turbofan Engines Aircraft Engines F-15 Aircraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
