An HTK-1 modified by the US Army and Navy by replacing the piston engine with a pair of Boeing 502-2 gas turbine engines, providing a combined power of 300 hp (224 kW) for continuous operation..

Overview

Data on design, manufacture and status

Design authority: Kaman Aircraft Corporation

Primary manufacturer: Kaman Aircraft Corporation

Parent type: Kaman K-225

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Synchropter (x2)

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: 2

Weights and Performance

Data on aircraft weight and flight characteristics

Related VFS Resources

Resources related to the HTK-1 (Twin-turbine) , provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the HTK-1 (Twin-turbine) , provided by public sources across the internet.

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