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Thesis Aviation The Speedster

thesis-speed

A staggerwing racer design with the upper wing flush with the fuselage top. First flown in 1995 and kits were available.

Engine: Kawasaki 440-A, 40 hp
HP range: 38-52
Height: 5 ft
Length: 13.7 ft
Wing span: 17.5 ft
Wing area: 77.5 sq.ft
Fuel capacity: 5 USG
Empty weight: 252 lb
Gross weight: 460 lb
Top speed: 75 mph
Cruise: 62 mph
Stall: 29 mph
Range: 125 sm
Rate of climb: 700 fpm
Takeoff dist: 150 ft
Landing dist: 200 ft
Seats: 1
Landing gear: tailwheel

 

 


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