Soviet Ultralight and Homebuilt Aircraft homebuilt aircraft assembly


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Mahaonas



Type single seat ultralight
Engine 15 hp
Propeller 2-blade wooden fixed 3,86 ft dia
Landing gear trigear
Length 16,3 ft
Wing Span 24,6 ft
Wing Area 90,5 sq.ft
Wing Aspect Ratio 6,6
Airfoil TSAGI P-II-16
Vertical Tail Area 6,7 sq.ft
Rudder Area 6,7 sq.ft
Horizontal Tail Area 13,3 sq.ft
Elevator Area 6,7 sq.ft
Empty Weight 190 lb
Gross Weight 369 lb
Wing Loading 4,07 lb / sq.ft
Power Loading 24,6 lb / hp
Fuel Capacity 1,5 gal
Top Speed 68 mph
Stall Speed 34 mph
Takeoff Roll n.a.
Rate of Climb 400 fpm
Bldg. Materials Wing: composite
Tail: tubing, fabric
Fuselage: tubing




3 view drawing




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