The Aero Resources J-2 of 1962 was a development of the Jovanovich J-2.
Designed by D K Jovanovich, it had stub wings supporting twin booms, twin tails. A three-blade rotor with articulated blades, was unpowered in horizontal flight.
Engine: 200hp Lycoming O-360-A2D
Rotor: diameter: 26’0″
Wingspan: 11’2″
Length: 16’0″
Useful load: 500 lb
Max speed: 122 mph
Cruise: 95 mph
Range: 200 mi
Ceiling: 10,000′.
Seats: 2
All Aero 