The Vought XSB3U was an American biplane scout bomber prototype that Vought-Sikorsky developed for the United States Navy in the 1930s. It was proposed as a conventional alternative to the monoplane XSB2U-1 that became the SB2U Vindicator, after the Navy's Bureau of Aeronautics issued a late 1934 specification for new scout bomber and torpedo bomber designs. The XSB3U was modified from the last production SBU Corsair, with the same airframe, a fully enclosed cockpit and a Pratt and Whitney R-1535 radial engine, but with a more streamlined surface and cowling and fully retractable landing gear. It reached Naval Air Station Anacostia in April 1936, together with its monoplane rival, and the tests showed the monoplane about 15 miles per hour faster, so the biplane was not developed. The Navy kept it for experimental and liaison work, and NACA used it at Langley Field for tail load tests from August 1938 to January 1939.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) EnginePratt & Whitney R-1535 radial engine 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
Source Vought XSB3U (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Vought XSB3U (Wikipedia)LeadQuote, Lead
The Vought XSB3U was an American biplane scout bomber developed by Vought-Sikorsky for the United States Navy during the 1930s.
Originated In
Also in Geography Atlas: where this subject originated.
Source Vought XSB3U (Wikipedia)Lead, nationalityQuote, Lead, nationality
The Vought XSB3U was an American biplane scout bomber developed by Vought-Sikorsky for the United States Navy during the 1930s.
Sources
1. Vought XSB3U (Wikipedia)
Operational history
The XSB3U-1 was delivered to Naval Air Station Anacostia for evaluation by the U.S. Navy in April 1936
Lead, nationality
The Vought XSB3U was an American biplane scout bomber developed by Vought-Sikorsky for the United States Navy during the 1930s.
Design and development, engine
and Pratt & Whitney R-1535 radial engine
Operational history, status
being retired shortly thereafter
Specifications (XSB3U-1), power
R-1535-82 radial engine, 750 hp (560 kW)
Specifications (XSB3U-1), empty weight
Empty weight: 3,876 lb (1,758 kg)
Specifications (XSB3U-1), gross weight
Gross weight: 5,837 lb (2,648 kg)
Specifications (XSB3U-1), speed
Maximum speed: 215 mph (346 km/h, 187 kn) at 8,900 feet (2,700 m)
Exemplifies: Aviation, Lead
The Vought XSB3U was an American biplane scout bomber developed by Vought-Sikorsky for the United States Navy during the 1930s.
In Group: Ground-Attack and Dive Bombers, Lead
The Vought XSB3U was an American biplane scout bomber developed by Vought-Sikorsky for the United States Navy during the 1930s.
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