Soviet Ultralight and Homebuilt Aircraft homebuilt aircraft assembly


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Antis



Type single-seat ultralight canard
Engine 25 hp
Propeller 2-blade wooden fixed 3,5 ft dia
Landing gear trigear
Length 20 ft
Wing Span 31,3 ft
Wing Area 170 sq.ft (with canard)
Wing Aspect Ratio n.a.
Airfoil n.a.
Vertical Tail Area n.a.
Rudder Area n.a.
Horizontal Tail Area n.a.
Elevator Area n.a.
Empty Weight 220 lb
Gross Weight 400 lb
Wing Loading 2,35 lb / sq.ft
Power Loading 16 lb / hp
Fuel Capacity n.a.
Top Speed 38 mph
Stall Speed 26 mph
Takeoff Roll n.a.
Rate of Climb n.a.
Bldg. Materials Wing: tubing, fabric
Tail: tubing, fabric
Fuselage: tubing




3 view drawing




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