The Douglas XB-31, also known as the Douglas Model 332, was Douglas's design for a very long range heavy bomber, submitted in response to the United States Army Air Forces request that also produced the Boeing B-29 Superfortress, the Lockheed XB-30 and the Consolidated B-32 Dominator. The request followed a 1939 committee report that recommended new long range heavy bombers, and the studies, for a bomber able to travel 5,000 miles, were approved on 2 December 1939. Through 1939 and 1940 Douglas studied the Model 332 with several engines, including the Wright R-2600, the Pratt and Whitney R-2800 and the Wright R-3350, which was the choice in the final Model 332F design of four Duplex-Cyclone radials of 2,200 horsepower each. The design carried a crew of eight and a wingspan of about 42.8 metres. It was rejected in favour of the B-29 and B-32 because the air corps judged the B-29 superior, so the XB-31 stayed a paper design.
Facts
Engine Class StatusDesign only (never built) 1 Top Speed (km/h) EngineWright R-3350-13 Duplex-Cyclone 18-cylinder radial piston engine 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
exemplifies recorded from the cited article.
Source Douglas XB-31 (Wikipedia)
Of Make
of-make recorded from the cited article.
Source Douglas XB-31 (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Douglas XB-31 (Wikipedia)Lead (manufacturer edge)Quote, Lead (manufacturer edge)
was the design submitted by Douglas after the request by the United States Army Air Forces
Originated In
Also in Geography Atlas: where this subject originated.
Source Douglas XB-31 (Wikipedia)Design and development (country-of-origin edge)Quote, Design and development (country-of-origin edge)
United States Army General Henry H. "Hap" Arnold, the head of the US Army Air Corps
Sources
1. Douglas XB-31 (Wikipedia)
Specifications (Model 332F as designed)
Maximum speed: 377 mph (607 km/h, 328 kn)
Specifications (Model 332F as designed), mass
Max takeoff weight: 120,000 lb (54,431 kg)
Specifications (Model 332F as designed), engine
Wright R-3350-13 Duplex-Cyclone 18-cylinder air-cooled radial piston engines
Lead (manufacturer edge)
was the design submitted by Douglas after the request by the United States Army Air Forces
Design and development (country-of-origin edge)
United States Army General Henry H. "Hap" Arnold, the head of the US Army Air Corps
Design and development (approval of design studies)
Approval was granted on 2 December 1939.
Lead
for a very heavy bomber aircraft
Design and development
The XB-31 design was rejected in favor of the B-29 and B-32
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