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Douglas XB-42 Mixmaster

Military Aircraft

The Douglas XB-42 Mixmaster was an experimental American bomber designed for a high top speed. Its unconventional approach was to mount the two engines within the fuselage and drive a pair of contra-rotating propellers at the tail in a pusher configuration, leaving the wing and fuselage clean and free of drag-inducing protrusions. The first of two prototypes was delivered to the Army Air Forces and flew at Palm Springs, California, on 6 May 1944, with performance basically as the original proposal described. The end of World War II changed priorities and the advent of the jet engine offered another route to high speed, so the type did not enter production.

Facts
Year
1944 1
Engine Class
Piston 1
Mass (kg)
9475 1
Maximum Mass (kg)
16,194 1
Comparison
Body Style
Aircraft (no road body style) 1
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Exemplifies

Aviation, Modes
Source Douglas XB-42 Mixmaster (Wikipedia)

Of Make

Source Douglas XB-42 Mixmaster (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Douglas XB-42 Mixmaster (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
The Douglas XB-42 Mixmaster is an experimental American bomber aircraft

Originated In

Also in Geography Atlas: where this subject originated.

Source Douglas XB-42 Mixmaster (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
The Douglas XB-42 Mixmaster is an experimental American bomber aircraft
Sources
1. Douglas XB-42 Mixmaster (Wikipedia)
  • Operational history
    flew at Palm Springs, California on 6 May 1944
  • Lead
    experimental American bomber aircraft
  • Specifications
    Allison V-1710-125 liquid-cooled V12 engines
  • Specifications, mass
    Empty weight: 20,888 lb (9,475 kg)
  • Specifications, maximum mass
    Max takeoff weight: 35,702 lb (16,194 kg)
  • Lead, manufacturer
    The Douglas XB-42 Mixmaster is an experimental American bomber aircraft
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