[1][2] The Meg-2XH Strap-On was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg).

The helicopter was designed to be powered by a single jet engine producing 37 hp (28 kW).

[1] The aircraft fuselage frame is made from bolted-together aluminum tubing and has a 21 ft (6.4 m) diameter two-bladed rotor.

With full fuel of 5 U.S. gallons (19 L; 4.2 imp gal) the maximum pilot weight is 250 lb (113 kg).

[1] The 5 U.S. gallons (19 L; 4.2 imp gal) fuel capacity gives the aircraft a range of 35 mi (56 km).