Soviet Ultralight and Homebuilt Aircraft

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Type single-seat ultralight biplane
Engine 40 hp
Propeller 2-blade wooden fixed 3,06 ft dia
Landing gear trigear
Length 16,2 ft
Wing Span 31,3 ft
Wing Area 111 sq.ft
Wing Aspect Ratio n.a.
Vertical Tail Area 16,2 sq.ft
Rudder Area 15,9 sq.ft
Horizontal Tail Area 17,4 sq.ft
Elevator Area 16,4 sq.ft
Empty Weight 297 lb
Gross Weight 475 lb
Wing Loading 4,28 lb / sq.ft
Power Loading 11,8 lb / hp
Fuel Capacity 2,6 gal
Top Speed 62 mph
Stall Speed 37 mph
Takeoff Roll 330 ft
Rate of Climb n. a.
Bldg. Materials Wing: metal, fabric
Tail: tubing, fabric
Fuselage: metal

3 view drawing n.a.