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SBU
Vought SBU-1.jpg
A SBU-1 of Scouting Squadron 41
Role Dive Bomber
National origin United States of America
Manufacturer Vought
Primary user United States Navy
Number built 125
Developed from Vought XF3U
Developed into Vought XSB3U

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 build any more two seat fighters. 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.

OperatorsEdit

Flag of Argentina.svg Argentina
United States

VariantsEdit

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

Specifications (SBU-1)Edit

Data from United States Navy Aircraft since 1911 [4]

General characteristics
  • Crew: two: pilot, navigator/gunner
  • Length: 27 ft 10 in (8.49 m)
  • Wingspan: 36 ft 3 in (10.14 m)
  • Height: 11 ft 11 in (3.63 m)
  • Wing area: 327 ft² (30.4 m²)
  • Empty weight: 3,645 lb (1,659 kg)
  • Max. takeoff weight: 5,520 lb (2,509 kg)
  • Powerplant: 1 × Pratt & Whitney R-1535-80 Twin Wasp Junior 14-cylinder two-row air-cooled radial engine, 700 hp (522 kW)

Performance

  • Maximum speed: 178 knots (205 mph, 330 km/h) at 8,900 ft (2,700 m)
  • Cruise speed: 106 knots (122 mph, 196 km/h)
  • Range: 477 naut mi (548 mi, 882 km)
  • Service ceiling: 23,700 ft (10,800 m)
  • Rate of climb: 1,180 ft/min (6.0 m/s)</ul>Armament
  • Guns: 1x Fixed forward firing .30 in (7.62 mm) Browning machine gun and 1x machine gun flexibly mounted .30 in machine gun in rear cockpit
  • Bombs: 1x 500 lb (227 kg) bomb
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ReferencesEdit

Notes
  1. Johnson 2008, p. 306.
  2. Andrade 1979, p.192
  3. 3.0 3.1 3.2 3.3 Andrade 1979, p.222
  4. Swanborough and Bowers 1976, p.396.
Bibliography

External linksEdit

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