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Sopwith Pup
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Sopwith Pup

Sopwith Pup
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Description
Role
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First Flight
Entered Service
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Length ft in m
Wingspan ft in m
Height ft in m
Wing Area ft²
Weights
Empty lb kg
Loaded lb kg
Maximum Takeoff lb kg
Capacity
Powerplant
Engines
Power hp kW
Performance
Maximum Speed mph km/h
Combat Range miles km
Ferry Range miles km
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Power/Mass hp/lb kW/kg
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The Sopwith Pup was a single seater biplane fighter aircraft used by the British in World War I. It was manufactured by the Sopwith Aviation Company and was officially named the Sopwith Scout. It was called the Pup because it looked like a smaller version of the Sopwith 1 1/2 Strutter.

The Pup was a highly regarded aircraft. It was pleasant to fly and was simple and reliable. Its large wings gave it a good rate of climb and agility. It was underpowered compared to the German Albatros DIII but could turn twice in the space of a single turn by an Albatros.

It was used to great effect by both the Royal Flying Corps and the Royal Naval Air Service. The first Pups reached the Western Front in October of 1916 and a total of 1,770 were built. After being removed from frontline service in mid-1917 they were used by a Home Defense squadron against Zeppelins. On August 2nd 1917, a Sopwith Pup flown by Sqn Cdr Edwin Dunning became the first aircraft to land aboard a moving ship, HMS Furious. Dunning was killed on his third landing when the Pup fell over the side of the ship.

The Pup was based on the personal plane of Sopwith's chief test pilot Harry Hawker. The Pup was powered by either an 80 or 100 horsepower (60 or 75 kW) air cooled rotary engine. It had a wing span of 26 ft 6 inches (8.1 m), a length of 19 ft 3.75 inches (5.9 m) and a height of 9 ft 5 inches (2.9 m). It weighed 856 pounds (388 kg) empty and 1,225 pounds (556 kg) when fully loaded. It's maximum speed was 106 mph (171 km/h) and it had a ceiling of 18,500 feet (5,600 m). It could fly missions of upto 3 hours in length.

It was armed with a single, forward firing Vickers 0.303 in (7.62 mm) machinegun. The machinegun fired forward through the propellor by means of an interrupter gear.
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