| Manufacturer |
McDonnell Douglas |
| Description |
The McDonnell Douglas F-15 STOL/MTD (Short Takeoff and Landing/Maneuver Technology Demonstrator) is a modified F-15 Eagle. |
| First Flight |
1988-09-07 |
| Service End |
1991-08-15 |
| Designer |
McDonnell Douglas |
| Type |
Technology Demonstrator and Research Aircraft |
| Length (m) |
19.42 |
| Height (m) |
5.64 |
| Cockpit Crew |
2 |
| Max Speed (km/h) |
2124.334 |
| Max Ceiling (m) |
18288 |
| Capacity Description |
17,000 lb (7,112 kg) |
| Max Mach (Mach) |
2 |
| National Origin |
United States of America |
| Number Built |
1 |
| Powerplant Description |
2 × Pratt & Whitney F100-PW-229 turbofan engines, equipped with 20° three-dimensional thrust vectoring P/YBBN, 79 kN thrust each |
| Primary Users |
United States Air Force, NASA |
| Status |
Retired from both NASA and military service |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/McDonnell_Douglas_F-15_STOL/MTD |
| Flat Wing Span (m) |
13 |
| Flat Wing Area (m²) |
56.5 |
| Aircraft Engine |
Pratt & Whitney F100 |
| Number of Engines |
2 |