[2][3][4] The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg).
It features a 290 sq ft (27 m2) Skybolt semi-elliptical or 450 sq ft (42 m2) Quantum Advantage rectangular parachute-style wing, single-seat accommodation, tricycle landing gear and a single 46 hp (34 kW) single carburetor Rotax 503 engine in pusher configuration.
In flight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.
The main landing gear incorporates spring and rod suspension.
[1][4] The prototype was configured with hand-only controls to allow it to be flown by paraplegic wheelchair aviators.