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
Engine Class Maximum Mass (kg) Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
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, manufacturerQuote, 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, manufacturerQuote, 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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