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
Top Speed (km/h) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
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
View the SourceReader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.
Sign in to dispute this or suggest a correction.