Soviet Ultralight and Homebuilt Aircraft homebuilt aircraft assembly


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I-2 impulse



Type 2-seat conventional low wing monoplane
Engine 2 x 35 hp
Propeller 2-blade wooden fixed 3,5 ft dia
Landing gear trigear
Length n.a.
Wing Span 23,7 ft
Wing Area 83,1 sq.ft
Wing Aspect Ratio 6,8
Airfoil NACA-23015
Vertical Tail Area 8 sq.ft
Rudder Area 3,1 sq.ft
Horizontal Tail Area 18,7 sq.ft
Elevator Area 7,55 sq.ft
Empty Weight 875 lb
Gross Weight 1330 lb
Wing Loading 16 lb / sq.ft
Power Loading 19 lb / hp
Fuel Capacity 18,6 gal
Top Speed n.a.
Stall Speed 68,7 mph
Takeoff Roll n.a.
Rate of Climb n.a.
Bldg. Materials Wing: n.a.
Tail: n.a.
Fuselage:n.a.




3 view drawing




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