Soviet Ultralight and Homebuilt Aircraft

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Type single-seat conventional ultralight
Engine 30 hp
Propeller 2-blade wooden fixed 4,4 ft dia
Landing gear trigear
Length 19,4 ft
Wing Span 31,6 ft
Wing Area 155 sq.ft
Wing Aspect Ratio 6,45
Airfoil n.a.
Vertical Tail Area 12,7 sq.ft
Rudder Area 12,7 sq.ft
Horizontal Tail Area 28,8 sq.ft
Elevator Area 9,77 sq.ft
Empty Weight 340 lb
Gross Weight 538 lb
Wing Loading 3,46 lb / sq.ft
Power Loading 17,9 lb / hp
Fuel Capacity 2,3 gal
Top Speed 50 mph
Stall Speed 34 mph
Takeoff Roll 200 ft
Rate of Climb 400 fpm
Bldg. Materials Wing: tubing, fabric
Tail: tubing, fabric
Fuselage: tubing

3 view drawing n.a.