The Fairey Jet Gyrodyne was a British experimental compound gyroplane built by the Fairey Aviation Company that combined features of the helicopter, gyrodyne and autogyro. It was the subject of a Ministry of Supply research contract to gather data for the Rotodyne, and was a modification of the second prototype FB-1 Gyrodyne, registered G-AJJP, built to develop the pressure-jet rotor drive and its operating procedures. It kept the fuselage, undercarriage and Alvis Leonides radial engine of the FB-1, which drove a pusher propeller at each wing tip and two superchargers, and its two-blade rotor was driven by air burned with fuel in tip pressure-jets for take-off, landing and low-speed flight. Tethered flights were followed by the first free flight in January 1954, and a full transition from helicopter to autogyro flight was achieved in March 1955. It was retired once ground testing of the Rotodyne rotor drive system began.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Fairey Jet Gyrodyne (Wikipedia)
Of Make
Source Fairey Jet Gyrodyne (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Fairey Jet Gyrodyne (Wikipedia)LeadQuote, Lead
The Fairey Jet Gyrodyne is a British experimental compound gyroplane built by the Fairey Aviation Company that incorporated helicopter, gyrodyne and autogyro characteristics.
Originated In
Also in Geography Atlas: where this subject originated.
Source Fairey Jet Gyrodyne (Wikipedia)LeadQuote, Lead
The Fairey Jet Gyrodyne is a British experimental compound gyroplane built by the Fairey Aviation Company that incorporated helicopter, gyrodyne and autogyro characteristics.
Sources
1. Fairey Jet Gyrodyne (Wikipedia)
Operational history
the first free flight in January 1954
Lead
The Fairey Jet Gyrodyne is a British experimental compound gyroplane built by the Fairey Aviation Company that incorporated helicopter, gyrodyne and autogyro characteristics.
Specifications (Jet Gyrodyne)
1 × Alvis Leonides 9-cylinder air-cooled radial piston engine, 520 hp (390 kW)
Specifications (Jet Gyrodyne), mass
Empty weight: 3,600 lb (1,633 kg)
Specifications (Jet Gyrodyne), maximum mass
Gross weight: 4,800 lb (2,177 kg)
Specifications (Jet Gyrodyne), top speed
Maximum speed: 140 mph (230 km/h, 120 kn)
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