The Bristol T.B.8, or Bristol-Coanda T.B.8 was an early British biplane designed by the Romanian Henri Coandă. Fifty-four Bristol T.B.8s were built, being mainly used as a trainer. A small number of Bristol T.B.8s were briefly used as bombers at the start of the World War I by the Royal Naval Air Service. Romanian Henri Coandă, chief designer of the Bristol Aeroplane Company, developed the Bristol T.B.8 as a biplane conversion of his previously designed Bristol-Coanda Monoplane. The conversion was made to meet an order from the British Admiralty, with the Bristol T.B.8 first flying on 12 August 1913. This aircraft was tested with both wheeled undercarriage and floats. The Bristol T.B.8 was a single-engine, two-seat biplane, with two-bay wings and a slender fuselage. It was powered by a variety of rotary engines, including the Gnome and Le Rhône engines with power ranging from 50 hp Gnomes to 100 hp Gnome Monosoupape. Early Bristol T.B.8s used wing warping, with later production aircraft being fitted with ailerons. Bristol T.B.8s were normally equipped with a distinctive four-wheel undercarriage. The Bristol T.B.8 was produced by both the conversion of existing Coanda-Bristol Monoplanes and the manufacturing of new aircraft. One Bristol T.B.8 was fitted with a prismatic Bombsight in the front cockpit and a cylindrical bomb carrier in the lower forward fuselage, capable of carrying twelve 10 lb (4.5 kg) bombs, which could be dropped singly or as a salvo as required. This aircraft was displayed at the Paris Salon de l’Aéronautique and evaluated by the French military before being purchased by the Royal Navy Air Service. Variants G.B.75 The Romanian government was pleased with the Bristol T.B.8 and placed an order for an improved version, for which they provided a 75 hp (56 kW) Gnome Monosoupape engine. The resulting aircraft, designated the G.B.75 was significantly different in appearance with a streamlined front fuselage and rounded cowling, enclosing the rotary engine. The characteristic Coanda fin was replaced with an unbalanced rudder plus fin. Maximum speed was increased to 80 mph (130 km/h). It first flew on 7 April 1914 and required the removal of the spinner and an increase in stagger to adjust the centre of pressure. Despite the alterations the Bristol G.B.75 was declared ready for service in June of 1914. The altered Bristol G.B.75s were requisitioned by the Royal Flying Corps at Farnborough, never being delivered to Romania, and being powered by a standard Gnome engine. T.B.8H One Bristol Coanda Monoplane was converted into the T.B.8 prototype and was fitted with twin floats as the T.B.8H “Hydro” variant. Specifications Crew 2 Length 29 ft 3 in (8.92 m) Wingspan 37 ft 8 in (11.48 m) Wing area 450 sq ft (42 m2) Empty weight 970 lb (440 kg) Gross weight 1,665 lb (755 kg) Powerplant 1 × Gnome Lambda,
7-cylinder air-cooled rotary piston engine, 80 hp (60 kW) Propellers 2-bladed fixed-pitch propeller Performance Maximum speed 65–70 mph (105–113 km/h, 56–61 kn) Endurance 5 hours Time to altitude 3,000 ft (914 m) in 11 minutes Armament Guns Some were equipped with a 7.92 machine gun. Bombs 12 x 10 lb (4.5 kg) light bombs.
