The final design in the proposed prototype program had a wingspan of 45 feet 10 inches, a length of 39 feet, and was configured as either a single or two-place airplane with zero-zero ejection capability. The turboprop engines considered were the 4,050hp Allison T-56-A7A and the GE 3,060hp CT64-820 (T-64). The basic (empty) weight of the T56-powered airplane was 17,300 lbs and the Design Gross Weight (takeoff weight) was 29,800 lbs, including 6,000lbs of external ordnance. The T-64 version was 15.395lbs and 26.350lbs respectively. These engines would drive a 13.5 foot fiberglass propeller.
The Model 100 offered two-hour loiter time at a 250 mile radius and a cruise speed of 320mph. It included a variety of survivability features including a heavily armored engine and cockpit area, duplicate components, fuel fire and explosion protection and failsafe structure design.