The Avian Gyroplane was a two-seat autogyro without wings, with a
ducted fan pusher propeller driven by a 200 hp (150 kW)
Lycoming IO-360 piston engine. It had a three-bladed
rotor, formed from bonded aluminium. There were
flapping hinges but no
drag hinges. In normal flight the rotor was undriven, but the design team were keen to enable vertical
jump starts, an autogyro technique which spins up the rotor before take off without forward movement over the ground. The first prototype used conspicuous tip jets fed directly with compressed air from a fuselage-mounted cylinder. The
fuselage was built on a light alloy box beam which carried the cabin, engine mounting, rotor pylon and propeller duct. The well-glazed cabin seated two in tandem in front of the engine. Entry was via a starboard-side door; dual controls were fitted.
Yaw was controlled with a rudder mounted within the propeller duct, enhancing its low-speed effectiveness. The Gyroplane had a fixed
tricycle undercarriage. The main wheels were mounted on steel cantilever legs and the nosewheel castered. ==Development history==