Also known by the following designations,

 

U.S. Army - H-23D

U.S. Navy - HTE-2

 

Source: "Helicopters from 'A to Z' ", Ralph P. Alex, AHS Newsletter, November 1961, Page 10

Overview

Data on design, manufacture and status

Design authority: Hiller Aircraft Corporation

Primary manufacturer: Hiller Aircraft Corporation

Parent type: No type defined

Aircraft status: Status unknown

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1

Crew seating: Side-by-side

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Lycoming Designation TBA (250 hp) reciprocating

Engine manufacturer: Lycoming Engines

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 1125 kg (2480 lb)

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