Vought SBU Corsair explained

The Vought SBU-1 Corsair was a two-seat, all-metal biplane dive bomber built by Vought Aircraft Company of Dallas, Texas for the US Navy. Its design was based upon the F3U-1 two-seat fighter that was abandoned when the Navy decided not to obtain any more two-seat fighters.

Design and development

The aircraft was equipped with a closed cockpit, had fixed landing gear, and was powered by a Pratt & Whitney R-1535 radial air-cooled engine as had the F3U-1, but also included a controllable pitch propeller and a new NACA cowl with adjustable cowling gills on the trailing edge of the cowl. The adjustable cowling gills permitted better control of cooling airflow over the engine.

The SBU-1 completed flight tests in 1934 and went into production under a contract awarded in January 1935. The Corsair was the first aircraft of its type, a scout bomber, to fly faster than 200 mph. The last SBU Corsairs were retired from active service in 1941, being reassigned as trainers.[1]

The name "Corsair" was used several times by Vought's planes; the O2U/O3U, SBU, F4U, and the A-7 Corsair II.

Operators

Variants

XF3U-1
  • Two-seat fighter prototype with a 700 hp R-1535-64 engine.[2]
    XSBU-1
  • The XF3U-1 converted to scout bomber prototype with a 700 hp R-1535-96 engine, later used as an engine test bed.
    SBU-1
  • Original production order; 84 aircraft with 750 hp R-1535-82 engine.
    SBU-2
  • Follow-on order; 40 aircraft with R-1535-98 engines.[3]
    Model V.142A
  • Export version for Argentina.

    Bibliography

    Notes and References

    1. Johnson 2008, p. 306.
    2. Andrade 1979, p. 192
    3. Andrade 1979, p. 222