McDonnell Douglas F-15 STOL/MTD
Total Fuel Capacity
6435.2
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All data (24 fields)
- Name
- McDonnell Douglas F-15 STOL/MTD
- 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