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 . The aircraft has a standard empty weight of . It features a single main rotor, a single fold-up seat and a
rudder. The aircraft is supported by a partial frame when on the ground, but take-off and landing are both accomplished by foot and the aircraft is worn like a
backpack, hence the name. The helicopter was designed to be powered by a single jet engine producing . The aircraft
fuselage frame is made from bolted-together
aluminum tubing and has a diameter two-bladed rotor. The aircraft has an empty weight of and a gross weight of , giving a useful load of . With full fuel of the maximum pilot weight is . The fuel capacity gives the aircraft a range of . It has a top speed of and a cruise speed of . The manufacturer estimated the construction time from the supplied bolt-together assembly kit as 30 hours. ==Operational history==