An aircraft composed of an airframe, an extending tail, a counter rotating, coaxial main rotor assembly including an upper rotor assembly and a lower rotor assembly, and a translational thrust system positioned at the extending tail. The translational thrust system provides translational thrust to the airframe. The aircraft includes a turn radius between about (595) feet and about (2440) feet for an airspeed between about (120) knots and about (210) knots at a constant altitude.
TURN RADIUS AND BANK ANGLE FOR ROTARY WING AIRCRAFT
2017-10-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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