Soviet Ultralight and Homebuilt Aircraft homebuilt aircraft assembly


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Expromt 200



Type single seat ultralight
Engine 25 hp
Propeller 2-blade wooden fixed 3,7 ft dia
Landing gear tailweel
Length 16 ft
Wing Span 24 ft
Wing Area 104 sq.ft
Wing Aspect Ratio 5,5
Airfoil TSAGI P-II-14
Vertical Tail Area 13,8 sq.ft
Rudder Area 7,3 sq.ft
Horizontal Tail Area 16,2 sq.ft
Elevator Area 8,1 sq.ft
Empty Weight 233 lb
Gross Weight 511 lb
Wing Loading 4,9 lb / sq.ft
Power Loading 20,4 lb / hp
Fuel Capacity 3,3 gal
Top Speed 94 mph
Stall Speed 31 mph
Takeoff Roll n.a.
Rate of Climb 300 fpm
Bldg. Materials Wing: tubing, composite, wood, fabric
Tail: tubing, fabric
Fuselage: tubing




3 view drawing




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