H-19C under the U.S. Army, HRS-1 under the US Navy.  By the glossary definition, with a Useful Load of 2250 lb (1021 kg), the calculated Empty Weight is approximately 2245 kg.

Overview

Data on design, manufacture and status

Design authority: Sikorsky Aircraft Corp.

Primary manufacturer: Sikorsky Aircraft Corp.

Parent type: Sikorsky S-55/H-19

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 (non-retractable)

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: P&W R-1340 reciprocating

Engine manufacturer: Pratt & Whitney

Take-off / rated power: 448 kW (600 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 3266 kg (7200 lb)

Max Range: 689 km (372 nm)

Related VFS Resources

Resources related to the S-55C (UH-19C, HRS-1), provided by the Vertical Flight Society.
Forum Proceedings
 
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.

Related Public Resources

Resources related to the S-55C (UH-19C, HRS-1), provided by public sources across the internet.

Images