Soviet Ultralight and Homebuilt Aircraft

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Type single-seat three surface ultralight
Engine 22 hp
Propeller 2-blade wooden fixed 2,83 ft dia
Landing gear trigear
Length 15,6 ft
Wing Span 18,6 ft
Wing Area 50 sq.ft
Wing Aspect Ratio 6,95
Airfoil TSAGI P-II-14
Vertical Tail Area n.a.
Rudder Area n.a.
Horizontal Tail Area 27,7 sq.ft
Elevator Area n.a.
Empty Weight 253 lb
Gross Weight 450 lb
Wing Loading 9 lb / sq.ft
Power Loading 20,4 lb / hp
Fuel Capacity 12,6 gal
Top Speed n.a.
Stall Speed 37,5 mph
Takeoff Roll n.a.
Rate of Climb 500 fpm
Bldg. Materials Wing: composite
Tail: composite
Fuselage: composite

3 view drawing