Overview
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.
Specifications
- Engine
- 2 × Bristol Hercules 734
- Engine type
- Piston
- Power
- 2 × 2,000 hp · 1,491 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 23
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 68 ft 4 in · 20.83 m
- Tail height
- 21 ft 8 in · 6.60 m
- Fuselage diameter
- 9 ft 6 in · 2.90 m
- Wing span
- 108 ft 0 in · 32.92 m
- Baggage volume
- 22,248 ft³ · 630.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 44,000 lb · 20,000 kg
- Max landing weight
- —
- 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
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 715 nm · 820 mi · 1,320 km
- Fuel burn
- —
- Ceiling
- 23,000 ft · 7,000 m
- Rate of climb
- 1,000 ft/min · 5 m/s
- Takeoff distance
- 2,500 ft · 760 m
- Landing distance
- 2,300 ft · 700 m
Gallery
Operational Context
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.
Sources and references used for research and fact-checking.