Trials in 1954, the aircraft flew; powered by two hydrogen peroxide rocket engines.

Overview

Data on design, manufacture and status

Design authority: Kellett Aircraft Corporation

Primary manufacturer: Kellett Aircraft Corporation

Parent type: No type defined

Aircraft status: Status unknown

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1

Crew seating: Single seater

Landing gear: Other

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

Max Gross Weight (ground): 292 kg (644 lb)

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Resources related to the KH-15 Stable Mabel, provided by public sources across the internet.

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