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Fairey Ultra-light Helicopter

Lighter-Than-Air Craft and Rotorcraft

The Fairey Ultra-light Helicopter was a small side-by-side two-seat helicopter designed for reconnaissance and casualty evacuation to a British Ministry of Supply requirement of 1953 for a low-cost rotorcraft that could travel on an Army three-ton truck. It had no tail rotor, because tip jets burning fuel at the ends of the rotor blades turned the rotor, fed with compressed air from a Blackburn built Turbomeca Palouste engine. The first prototype flew on 14 August 1955 and appeared at the Farnborough show that September. The type fell victim to defence economies and competition from the Saunders-Roe Skeeter, no orders came, and Fairey shelved it to concentrate on the Rotodyne.

Facts
Year
1955 1
Engine Class
Jet 1
Status
Cancelled 1
Maximum Mass (kg)
816.5 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Source Fairey Ultra-light Helicopter (Wikipedia)

Of Make

Source Fairey Ultra-light Helicopter (Wikipedia)
Sources
1. Fairey Ultra-light Helicopter (Wikipedia)
  • Lead
    The Fairey Ultra-light Helicopter was a small British military helicopter intended to be used for reconnaissance and casualty evacuation
  • Operational history
    On 14 August 1955, the first prototype Ultra-light helicopter conducted its maiden flight.
  • Design
    powered by a single Turbomeca Palouste turbojet engine, which was produced under licence by Blackburn
  • Lead, status
    The firm shelved the project, choosing to concentrate on the larger Fairey Rotodyne instead
  • Specifications
    Gross weight: 1,800 lb (816 kg)
  • Lead, manufacturer
    designed by the Fairey Aviation Company
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