A variant of the US Army H-2 Tomahawk, fitted with wings and a pair of GE YJ85 turbojet pods on either side of the fuselage; the exact engine model is unknown.

Overview

Data on design, manufacture and status

Design authority: Kaman Aircraft Corporation

Primary manufacturer: Kaman Aircraft Corporation

Parent type: Kaman K-800/H-2 Seasprite

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Compound Helicopter

Compound type: Lift and Thrust compounded with 2 propulsors

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: TBA in Side-by-side arrangement

Landing gear: Wheels (some retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

References

References and sources used

Helicopters & Autogyros of the World
Paul Lambermont, Anthony Pirie
Cassell & Company Ltd., 1959 (page 320)
Book

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Resources related to the H-2 Tomahawk (Compound), provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the H-2 Tomahawk (Compound), provided by public sources across the internet.

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