Soviet Ultralight and Homebuilt Aircraft homebuilt aircraft assembly


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Etud



Type single-seat conventional high wing monoplane
Engine 30 hp
Propeller 2-blade wooden fixed 5 ft dia
Landing gear trigear
Length 16,9 ft
Wing Span 25,6 ft
Wing Area 94,4 sq.ft
Wing Aspect Ratio 7
Airfoil NACA-6412
Vertical Tail Area 10,5 sq.ft
Rudder Area 6,33 sq.ft
Horizontal Tail Area 17,8 sq.ft
Elevator Area 7,1 sq.ft
Empty Weight 373 lb
Gross Weight 593 lb
Wing Loading 6,28 lb / sq.ft
Power Loading 19,7 lb / hp
Fuel Capacity 5,3 gal
Top Speed 75 mph
Stall Speed 44 mph
Takeoff Roll n.a.
Rate of Climb 400 fpm
Bldg. Materials Wing: wood
Tail: wood, metal
Fuselage: metal




3 view drawing




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