Vought SBU Corsair
| SBU | |
|---|---|
 |
|
| A SBU-1 of Scouting Squadron 41 | |
| Role | Dive Bomber |
| National origin | United States of America |
| Manufacturer | Vought |
| First flight | May 1933 |
| 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.
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.[3]
- SBU-1
- Original production order; 84 aircraft with 750 hp 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)
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)
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
References
- Notes
<templatestyles src="Reflist/styles.css" />
Cite error: Invalid <references> tag; parameter "group" is allowed only.
<references />, or <references group="..." />- Bibliography
- Lua error in package.lua at line 80: module 'strict' not found.
- Lua error in package.lua at line 80: module 'strict' not found.
- Swanborough, Gordon and Bowers, Peter M. United States Navy Aircraft since 1911. London:Putnam, 1976. ISBN 0-370-10054-9.
External links
Media related to Lua error in package.lua at line 80: module 'strict' not found. at Wikimedia Commons
