F-15 STOL/MTD
The McDonnell Douglas F-15 STOL/MTD (Short Takeoff and Landing/Maneuver Technology Demonstrator) is a modified F-15 Eagle. Developed as a technology demonstrator, the F-15 STOL/MTD carried out research for studying the effects of thrust vectoring and enhanced maneuverability. The aircraft used for the project was pre-production TF-15A (F-15B) No. 1 (USAF S/N 71-0290), the first two-seat F-15 Eagle built by McDonnell Douglas (out of 2 prototype), the sixth F-15 off the assembly line, and was the oldest F-15 flying up to its retirement. It was also used as the avionics testbed for the F-15E Strike Eagle program. The plane was on loan to NASA from the United States Air Force.
Tip:
For STOL,and Flying,Please use trim control to have a better pitch
Specifications
General Characteristics
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- Wingspan 33.3ft (10.2m)
- Length 40.6ft (12.4m)
- Height 13.4ft (4.1m)
- Empty Weight 26,832lbs (12,171kg)
- Loaded Weight 32,583lbs (14,779kg)
Performance
- Power/Weight Ratio 2.255
- Wing Loading 82.7lbs/ft2 (403.5kg/m2)
- Wing Area 394.2ft2 (36.6m2)
- Drag Points 4598
Parts
- Number of Parts 75
- Control Surfaces 8
- Performance Cost 501