Star-Lite Warp 1-A

[1] 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).

[1] The Warp 1-A features a cantilever mid-wing, a single-seat enclosed cockpit under a bubble canopy, fixed tricycle landing gear with wheel pants, a boom-mounted T-tail and a single pod-mounted engine in pusher configuration.

With full fuel of 5 U.S. gallons (19 L; 4.2 imp gal) the payload for the pilot and baggage is 295 lb (134 kg).

[1][2] The standard day, sea level, no wind, take off and landing roll with a 50 hp (37 kW) engine is 150 ft (46 m).

[1] In March 2014 one example, the prototype, was registered in the United States with the Federal Aviation Administration as an Experimental - Amateur-built, although its registration expired in June 2013.