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 160NaN0 motor with a 2.5:1 ratio reduction drive and a 1230NaN0 diameter two-bladed wooden propeller. Later versions feature a Cors'Air M21Y 250NaN0 motor and a 1240NaN0 diameter two-bladed wooden propeller. The fuel tank capacity is, while later versions offer an option of . The aircraft is built in two versions, one predominantly from aluminium and the other from titanium.[1] [2]
As is the case with all paramotors, take-off and landing is accomplished by foot. Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.[1]