The Solo 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 140NaN0 Solo 210 engine in pusher configuration with a reduction drive and a 1100NaN0 diameter three-bladed composite German Helix-Carbon propeller. The fuel tank capacity is . The aircraft backpack chassis is built so that it can be quickly disassembled into five parts for ground transport and storage.[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.[1]