The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules.
It features a rectangular paraglider-style wing, single-place accommodation and a single 22 hp (16 kW) Zenoah G-25 engine in pusher configuration, with recoil start.
As is the case with all paramotors, take-off and landing is accomplished by foot.
The smaller is 315 sq ft (29.3 m2) area for pilots up to 175 lb (79 kg) and the larger 360 sq ft (33 m2) area for pilots up to 220 lb (100 kg).
[1] The aircraft can be modified into a powered parachute by the addition of a wheeled cart that mounts the engine package.