Bell HUL-1M
This was an experimental aircraft based on a Model 47-J, modified to include the Allison T63 turbine engine. The useful load is 1500 lb (680 kg).
.jpg "Photo from Vertiflite, January/February 1974 courtesy of AHS International (image cropped from original)")
Overview
Data on design, manufacture and statusDesign authority: Bell Helicopter Textron, Inc.
Primary manufacturer: Bell Helicopter Textron, Inc.
Parent type: No type defined
Aircraft status: No longer flying
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift devices: 1 Single main rotor
Dedicated control device: 1 Tail rotor
Crew required: 1 in Side-by-side arrangement
Landing gear: Skids
Key Characteristics
Data on key physical featuresAircraft Details
Data on aircraft configuration, weights, flight performance and equipmentReferences
References and sources used
Helicopters from "A to Z" | Part I
Ralph P. Alex
AHS Newsletter, 1961, October, 1961 (page 6)
Periodical
AHS Newsletter, 1961, October, 1961 (page 6)
Periodical
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