Bristol Aeroplane Company · United Kingdom · 1945–1958

The Bristol Type 170 Freighter was a twin-engine aircraft manufactured by the British Bristol Aeroplane Company. It was designed as a freighter and an airliner and was well-known as an air ferry to transport cars and their passengers on fairly short ranges.

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Engine:
2× Bristol Hercules 734
Engine type:
Piston
Power:
2 × 2,000 hp  ·  1,491 kW
Wing Tips:
No winglets
Seats:
23
Exterior length:
68 ft 4 in · 20.83 m
Tail height:
21 ft 8 in · 6.60 m
Fuselage diameter:
ft 6 in · 2.90 m
Wing span / rotor:
108 ft 0 in · 32.92 m
Baggage volume:
22,248 ft³  ·  630.0 
Max takeoff weight:
44,000 lb  ·  20,000 kg
Max Payload:
16,200 lb  ·  7,350 kg
Fuel capacity:
1,170 gal  ·  4,400 L  ·  3,200 kg  (AvGas)
Max cruise speed:
196 kt  ·  226 mph  ·  363 km/h
Range:
715 nm  ·  820 mi  ·  1,320 km
Ceiling:
23,000 ft  ·  7,000 m
Rate of climb:
1,000 ft/min  ·  m/s
Takeoff distance:
2,500 ft  ·  760 m
Landing distance:
2,300 ft  ·  700 m
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The Bristol Type 170 Freighter was a high mounted-wing monoplane built particularly for the economic transport of freight by air. The Type 170 Freighter was a well-defined aircraft, designed with a box-shaped fuselage with an external length of 20.83 meters, a diameter of 2.9 meters, and a height of 6.6 meters. It also has a circular nose and a high-set flight deck.

So as to achieve the best economical performance, adjustments were made on the performance which resulted in a comparatively low cruising speed, which was not seen as an important factor in a freighter’s role and as well as not a vital diminishing element. The Freighter also featured two big clamshell doors to easily enter the main hold, and because of this layout, the unpressurized fuselage was a bit airy in flight.

The aircraft was proposed to be operated on low speeds and high-frequency short-distance routes. The high-mounted wing and fixed landing gear were thought to be unusual at that time and developed in higher drag compared to a low-mounted wing. The main gear legs were equipped with shock absorbers manufactured by Dowty Group and were strengthened by a configuration of reinforced vertical struts situated further down the engines and underneath the edge of the fuselage. The aircraft has a wheelbase of 14 meters, a wingspan of 32.92 meters, and a wing area of 138.1 square meters

The Bristol Fighter was powered by two Bristol Hercules 734 piston engines with a maximum thrust of 2,000 horsepower each. It was a 14-cylinder, two-row, supercharged, air-cooled radial engine with gear-driven sleeve valves, single-speed centrifugal-type supercharger, Claudel-Hobson carburetor, and a Farman epicyclic gearing. The aircraft was also equipped with four-bladed constant-speed fully-feathering metal propellers built by de Havilland.

The aircraft has a maximum speed of 196 knots at 3,000 feet and a travel range of 710 nautical miles with 5,400 kg of payload. It has a maximum takeoff weight of 19,958 kg.

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