Developed in 1945. The initial prototype had only the frame; the final version of 1946 has a closed fuselage.
Design authority: Bendix Helicopters Inc.
Primary manufacturer: Bendix Helicopters Inc.
Parent type: No type defined
Aircraft status: No longer flying
VTOL type: Helicopter
Lift devices: 2 in Coaxial configuration
Crew required: 1 in Single seater arrangement
Landing gear: Wheels (non-retractable)