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Magni M20 Talon

magni_m-20


A single-seat autogyro ultralight, prototypes were flying but production had not begun by mid-2003, although promotion was continuing.
Featuring a pod and boom fuselage with sweptback tailplane and triple fins, the rudder is on the central fin only. The M 18 Spartan can he upgraded to M 20 standard.
A welded 4130 chromoly main structure with glass fibre fuselage and wheel fairings, and two-blade main rotor of composites construction with mechanical prerotator. The landing gear is a fixed tricycle type.
Power is from one 59.6kW Rotax 912 UL flat-four driving a ground-adjustable pitch, three-blade, carbon fibre pusher propeller. Fuel in integral cockpit seat/tank of epoxy/glass fibre, capacity 45 litres.

Magni M 20 Talon
Engine: 59.6kW Rotax 912 UL
Rotor diameter: 7.62m
Overall length: 3.92m
Overall width: 1.73m
Overall height: 2.37m
Propeller diameter: 1.62m
Weight empty: 205kg
Max take-off weight: 300kg
Max level speed: 177km/h
Cruising speed: 145km/h
Rate of climb at sea level: 300m/min
Service ceiling: 3500m
Take-off run: 45m
Landing run: up to 30m
Range, no reserves: 289km
Endurance: 3 hr

 

 


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