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Gloster Goral

Military Aircraft

The Gloster Goral was a single-engined, two-seat biplane built to Air Ministry specification 26/27 for a general-purpose military aircraft in the late 1920s. The specification encouraged reuse of surplus Airco DH.9A wings and a metal airframe for overseas service, and at least eight manufacturers responded. Gloster built an all-metal framed, fabric-covered biplane with two-bay DH.9A wings and an uncowled 425 horsepower Bristol Jupiter VIA radial, and the pilot sat ahead of a gunner with a ring-mounted gun. It first flew in February 1927 but lost the contest to the Westland Wapiti and only one was built, despite Argentine interest as late as 1931.

Facts
Year
1927 1
Status
One-off concept 1
Top Speed (km/h)
219 1
Mass (kg)
1268 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Gloster Goral (Wikipedia)

Of Make

Source Gloster Goral (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Gloster Goral (Wikipedia)Lead and development, maker
Quote, Lead and development, maker
the Goral was Gloster's submission
Sources
1. Gloster Goral (Wikipedia)
  • Development, first flight
    almost immediately after its first flight in February 1927
  • Lead, aircraft
    a general-purpose military aircraft in the late 1920s
  • Lead, only one built
    It did not win the contest and only one was built.
  • Specifications, maximum speed
    Maximum speed: 136 mph (218 km/h, 118 kn) at 5,000 ft (1,500 m)
  • Specifications, empty weight
    Empty weight: 2,796 lb (1,268 kg)
  • Lead and development, maker
    the Goral was Gloster's submission
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