The HTE-1 was the U.S. Navy training version of the Hiller Model 360, with tricycle landing gear.

Overview

Data on design, manufacture and status

Design authority: Hiller Aircraft Corporation

Primary manufacturer: Hiller Aircraft Corporation

Parent type: Hiller Model 360

Aircraft status: No longer flying

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: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Franklin O-335-4 reciprocating

Engine manufacturer: Franklin Engine Company

Take-off / rated power: 133 kW (178 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 953 kg (2100 lb)

Max Range: 209 km (113 nm)

Related VFS Resources

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Related Public Resources

Resources related to the HTE-1 , provided by public sources across the internet.

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