Soviet Ultralight and Homebuilt Aircraft homebuilt aircraft assembly


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M-3



Type 2-seat conventional high wing monoplane
Engine 100 hp
Propeller 2-blade wooden fixed 6,7 ft dia
Landing gear tailweel
Length 27 ft
Wing Span 46 ft
Wing Area 230 sq.ft
Wing Aspect Ratio 9,2
Airfoil NACA 4312
Vertical Tail Area 22,2 sq.ft
Rudder Area 18,3 sq.ft
Horizontal Tail Area 34,4 sq.ft
Elevator Area 14,4 sq.ft
Empty Weight 1077 lb
Gross Weight 1528 lb
Wing Loading 6,64 lb / sq.ft
Power Loading 15,3 lb / hp
Fuel Capacity 9,3 gal
Top Speed 87 mph
Stall Speed 31 mph
Takeoff Roll n.a.
Rate of Climb 600 fpm
Bldg. Materials Wing: metal, fabric
Tail: metal, fabric
Fuselage: metal




3 view drawing




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