C-141 Starlifter Flaps experiment
25.2k JacobHardy64
9.7 years ago
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Auto Credit Based on SemedianIndustries's Semedian C141 Starlifter
SemedolasPT's C-141 modified. Rotator flaps versus Yaw Flaps instead of rudder. with both deployed, this plane has halfway decent STOL (Short Takeoff Or Landing) capabilities. Note: group 1 to activate nose wheel, THERE IS NO RUDDER CONTROL SURFACE!
Try stalling, taking off, landing, etc and tell me what you think. your reviews will help future technology of my modified aircraft!
Rate, comment, share, and feel free to point out mistakes. Good luck!
Specifications
General Characteristics
- Predecessor Semedian C141 Starlifter
- Created On Mac
- Wingspan 83.4ft (25.4m)
- Length 63.0ft (19.2m)
- Height 15.6ft (4.8m)
- Empty Weight 10,854lbs (4,923kg)
- Loaded Weight 18,653lbs (8,460kg)
Performance
- Power/Weight Ratio 0.722
- Wing Loading 24.1lbs/ft2 (117.5kg/m2)
- Wing Area 775.4ft2 (72.0m2)
- Drag Points 5565
Parts
- Number of Parts 357
- Control Surfaces 12
- Performance Cost 896
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