Developed in 1953, designated YHO-3BR in the US Army.  A two-seat helicopter with wheel-skid combination landing gear.  As the maiden flight, the first prototype flew in 1943; the second prototype flew in 1946 before the B-2 received its FAA certification [Ref 312].

Overview

Data on design, manufacture and status

Design authority: Brantly Helicopter Corp.

Primary manufacturer: Brantly Helicopter Corp.

Parent type: No type defined

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 1-2 in Side-by-side arrangement

Landing gear: Other

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

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