By the glossary definition, with a Useful Load of 8323 lb (3775 kg), the calculated Empty Weight is approximately 6226 kg.

Overview

Data on design, manufacture and status

Design authority: Sikorsky Aircraft Corp.

Primary manufacturer: Sikorsky Aircraft Corp.

Parent type: Sikorsky S-61/H-3

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: TBA

Crew seating: Side-by-side

Landing gear: Wheels (some retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: GE T58-GE-5 turbine

Engine manufacturer: General Electric Company

Max continuous power: 933 kW (1250 hp)

Take-off / rated power: 1119 kW (1500 hp)

Intermediate power: 1044 kW (1400 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 10002 kg (22050 lb)

Max Range: 1250 km (675 nm)

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Resources related to the S-61R (HH-3F) , provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the S-61R (HH-3F) , provided by public sources across the internet.

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