It had an enclosed structure for one pilot and an 85 hp (63 kW) radial engine driving two rotors, each rotor fitted to a short boom on each side of the fuselage.
The H-2 first flew on 2 November 1944 and the company was awarded a development contract by the United States Army.
It was not developed or bought and the company ceased operations by the end of the 1940s.
[1] Control of blade pitch was also unconventional, with the blade shells rotating freely about the spars, controlled by ailerons near the tips.
Aircraft of comparable role, configuration, and era