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Gloster Goring

Military Aircraft

The Gloster Goring was a single-engined, two-seat biplane built to Air Ministry specifications issued in 1926 for a day and torpedo bomber, for which several makers entered prototypes. It had staggered, unequal-span wings, a wooden fuselage of rectangular section, a pilot under a cut-out in the upper wing and a gunner with a Scarff-ring gun who could lie prone for bombing, and it could carry torpedoes on a split-axle undercarriage or operate as a seaplane. It first flew in March 1927 with a Bristol Jupiter VI engine. At Martlesham Heath in 1928 it competed against the Hare, Harrier and Witch without winning an order, and the single aircraft later served as an engine testbed at Bristol Filton works.

Facts
Year
1927 1
Status
One-off concept 1
Top Speed (km/h)
219 1
Mass (kg)
1322 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Gloster Goring (Wikipedia)

Of Make

Source Gloster Goring (Wikipedia)
Sources
1. Gloster Goring (Wikipedia)
  • Development, first flight
    The Goring originally flew in March 1927
  • Lead, aircraft
    single-engined two-seat biplane
  • Lead, one aircraft built
    the one aircraft built served later as an engine testbed
  • Specifications, maximum speed
    Maximum speed: 136 mph (218 km/h, 118 kn) at 4,000 ft (1,219 m)
  • Specifications, empty weight
    Empty weight: 2,914 lb (1,321 kg)
  • Lead and development, maker
    Goring was Gloster's submission
  • In Group: Bombers, Lead, aircraft role
    for a day/torpedo bomber
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