Developed in 1958, powered by two air bleed turbine engines and equipped with a rudder on the tail, using the exhaust to steer.
Design authority: Monte-Copter, Inc.
Primary manufacturer: Monte-Copter, Inc.
Parent type: No type defined
Aircraft status: No longer flying
VTOL type: Helicopter
Lift devices: 1 Single main rotor
Dedicated control device: 1 Rudder
Crew required: 1 in Side-by-side arrangement
Landing gear: Wheels (non-retractable)