[1] The Pegasus was designed to comply with the US FAR 103 Ultralight Vehicles rules as well as European regulations.
It features a paraglider-style wing, single-place accommodation and a single engine in pusher configuration.
Early versions were powered by a Solo 210 16 hp (12 kW) motor with a 2.5:1 ratio reduction drive and a 123 cm (48 in) diameter two-bladed wooden propeller.
Later versions feature a Cors'Air M21Y 25 hp (19 kW) motor and a 124 cm (49 in) diameter two-bladed wooden propeller.
Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.