MIG-8 UTKA
It's an experimental aircraft wing (high wing) Soviet. Built of wood, the plane was designed and built in 1945 to test the new canard configuration. It also uses a tricycle undercarriage, which was first used by the design bureau (OKB). It was modified to test various configurations and vertical stabilizer wing tip and then used as a liaison aircraft for years by the design bureau. N has the nickname "Utka" ( "duck"), from which the name Similar to duck in French, "canard", for a small additional wing at the front of the plane and the surface of the main undercarriage in the rear of the fuselage. Behind canard design is unique because it has a propeller. This aircraft five-cylinder radial engine Shvetsov M-11 with a propeller thrusters. This aircraft is used as a test aircraft for the development of air with bent wing MiG-15 aircraft and later used as a communication / versatile by OKB. Made of wood and fabric, this plane is very light and is a favorite MiG test pilots for docility and low speed characteristics. Wikipedia
Specifications
General Characteristics
- Successors 2 airplane(s)
- Created On Windows
- Wingspan 35.4ft (10.8m)
- Length 28.2ft (8.6m)
- Height 11.0ft (3.4m)
- Empty Weight 8,365lbs (3,794kg)
- Loaded Weight 11,057lbs (5,015kg)
Performance
- Horse Power/Weight Ratio 0.09
- Wing Loading 42.0lbs/ft2 (205.2kg/m2)
- Wing Area 263.0ft2 (24.4m2)
- Drag Points 2425
Parts
- Number of Parts 38
- Control Surfaces 8
- Performance Cost 246
iya. trimakasih @ccooper. Saya beruntung mendapat gambar contekan hasil browsing di google.
the trim on cannard need some adjustment