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Douglas DC-8 (piston airliner)

Airliners and Commercial Jet Aircraft

The Douglas DC-8 was a piston-engined airliner project of the Douglas Aircraft Company, conceived shortly after the end of World War II, more than a decade before the DC-8 jetliner. Based on the cancelled XB-42, it was meant to serve short and medium range routes with 40 to 48 passengers in a pressurized cabin. Two Allison V-1710 engines fitted below and behind the cockpit were to drive contra-rotating propellers in the tail through driveshafts under the cabin floor, an arrangement that promised to cut drag by 30 percent and avoid the control problems of an engine failure on a conventional twin. Excessive complexity and high development costs meant that airlines preferred less risky types such as the Convair 240 and the Martin 2-0-2, and the project was dropped before a prototype was built.

Facts
Engine Class
Piston 1
Status
Cancelled 1
Top Speed (km/h)
450 1
Mass (kg)
11,074 1
Maximum Mass (kg)
18,144 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Douglas DC-8 (piston airliner) (Wikipedia)

Of Make

Source Douglas DC-8 (piston airliner) (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Douglas DC-8 (piston airliner) (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
piston-engined airliner project by Douglas Aircraft

Originated In

Also in Geography Atlas: where this subject originated.

Source Douglas DC-8 (piston airliner) (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
an American piston-engined airliner project by Douglas Aircraft
Sources
1. Douglas DC-8 (piston airliner) (Wikipedia)
  • Lead
    piston-engined airliner project
  • Specifications (estimated)
    Allison V-1710-G4L/R liquid-cooled V12 engine
  • Lead, status
    The airliner project was canceled after development costs made it commercially unviable.
  • Specifications (estimated), mass
    Empty weight: 24,415 lb (11,074 kg)
  • Specifications (estimated), maximum mass
    Gross weight: 40,000 lb (18,144 kg)
  • Specifications (estimated), top speed
    Maximum speed: 280 mph (450 km/h, 240 kn) at 20,200 ft
  • Lead, manufacturer
    piston-engined airliner project by Douglas Aircraft
  • Lead, country of origin
    an American piston-engined airliner project by Douglas Aircraft
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