Soviet Ultralight and Homebuilt Aircraft homebuilt aircraft assembly


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Ptenetz



Type single seat ultralight
Engine 22 hp
Propeller 2-blade wooden fixed 3,4 ft dia
Landing gear trigear
Length 18,4 ft
Wing Span 28,6 ft
Wing Area 114,4 sq.ft
Wing Aspect Ratio 7,2
Airfoil n.a.
Vertical Tail Area 12,2 sq.ft
Rudder Area 11,9 sq.ft
Horizontal Tail Area 17,7 sq.ft
Elevator Area 7,8 sq.ft
Empty Weight 184 lb
Gross Weight 346 lb
Wing Loading 3,02 lb / sq.ft
Power Loading 15,7 lb / hp
Fuel Capacity 3 gal
Top Speed 72 mph
Stall Speed 28 mph
Takeoff Roll n.a.
Rate of Climb 700 fpm
Bldg. Materials Wing: tubing, fabric
Tail: tubing, fabric
Fuselage: tubing




3 view drawing




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