It was intended 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 14 hp (10 kW) Radne Raket 120 engine in pusher configuration with a 3:1 ratio reduction drive, recoil start and a 95 cm (37 in) diameter three-bladed, ground adjustable, composite propeller.
The aircraft chassis is built from a combination of high-tensile steel.
[1] 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.