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Auto Credit Based on Onat67's TUSAS ANKA-S (Reupload,Better Version)
The assembly and production of the Turkish Unmanned Aerial Vehicle "ANKA", designed by Turkish Aerospace Engineers and in which many domestic subcontractors took part, was completed and left the hangar with a ceremony held at the Turkish Aerospace Industries facilities on July 16, 2010. ANKA, whose engine is also started after leaving the hangar, aims to be the best operative system in the world in its category. A serial production contract (ANKA-S) for 10 aircraft was signed in October 2013 for the ANKA Unmanned Aerial Vehicle System, which made its first flight on 30 December 2010. The work in the ANKA-S Project has been successfully completed.
Specifications
General Characteristics
- Predecessor TUSAS ANKA-S (Reupload,Better Version)
- Created On Android
- Wingspan 148.7ft (45.3m)
- Length 78.5ft (23.9m)
- Height 27.0ft (8.2m)
- Empty Weight 41,968lbs (19,036kg)
- Loaded Weight 55,572lbs (25,207kg)
Performance
- Power/Weight Ratio 0.606
- Horse Power/Weight Ratio 0.044
- Wing Loading 30.1lbs/ft2 (147.1kg/m2)
- Wing Area 1,844.4ft2 (171.4m2)
- Drag Points 19855
Parts
- Number of Parts 159
- Control Surfaces 2
- Performance Cost 748
In my old designs, I preferred to keep the sizes large in order to make more precise sizing. @cattenowo
Why is this so unnecessarily big
Yes again
Because previous one's propeler's invert is wrong (: