F-15 stol/mtd aoa research vehicle 4
618 Myplanes
6.2 years ago
No Tags
Auto Credit Based on Myplanes's Post-stall / flat spin recovery research demonstrator
Thrust vectoring in the pitch, yaw, and roll axes. Canards for roll control at high angles of attack.
Specifications
General Characteristics
- Predecessor Post-stall / flat spin recovery research demonstrator
- Created On iOS
- Wingspan 37.5ft (11.4m)
- Length 54.0ft (16.5m)
- Height 17.1ft (5.2m)
- Empty Weight 14,605lbs (6,625kg)
- Loaded Weight 16,592lbs (7,526kg)
Performance
- Power/Weight Ratio 4.063
- Wing Loading 16.6lbs/ft2 (81.2kg/m2)
- Wing Area 998.1ft2 (92.7m2)
- Drag Points 4420
Parts
- Number of Parts 59
- Control Surfaces 6
- Performance Cost 513
one of the engines set fire while i was decreasing speed
What do you plan to do with the things you learn?