The design meets the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg) and has also been certified in the German 120 kg class.

It features a cable-braced hang glider-style high-wing, weight-shift controls, a single-seat open cockpit without a cockpit fairing, tricycle landing gear without wheel pants and a single engine in pusher configuration.

[1] The ANT is supplied with a carrying bag into which the aircraft fuselage frame can be stowed for ground transport by automobile, after folding up the airframe.

The wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar.

The powerplant is a single-cylinder, air-cooled, two-stroke, single-ignition 25 hp (19 kW) Cors-Air M25Y engine, normally used for powered paragliders.