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 devices: 2 in Synchropter configuration

Crew required: 1 in Side-by-side arrangement

Landing gear: Wheels (non-retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

Related VFS Resources

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