| By the spring of 1931, several months of operation of the
Curtiss F8C-4 aboard the USS Saratoga had proved conclusively
that this type was unsatisfactory in the fleet
fighter role. As a consequence, the US Navy's BuAer reformulated
its two-seat fighter requirement, and, from
seven proposals received in April 1932, those of Vought
and Douglas were selected, contracts being signed on
30 June 1932 for one prototype of each as the XF3U-1
and XFD-1 respectively. The XF3U-1 was flown on 9
May 1933, and was of all-metal construction with fabric
skinning apart from the metal-covered fixed tail surfaces.
Powered by a 14-cylinder Pratt & Whitney
R-1535-64 Twin Wasp Junior geared and supercharged
engine rated at 700hp at 2715m, the XF3U-1
had an armament of two 7.62mm cowl guns
and a third gun of similar calibre on a flexible mounting
in the rear cockpit. It demonstrated a marginal performance
superiority over the competitive XFD-1, but the
BuAer had meanwhile lost interest in the two-seat
fighter category, and, in November 1933, it was decided
to adapt the XF3U-1 for the scout-dive bomber role as
the XSBU-1.
 | A three-view drawing (1278 x 980) |
WEIGHTS |
Take-off weight | 2313 kg | 5099 lb |
Empty weight | 1558 kg | 3435 lb |
DIMENSIONS |
Wingspan | 9.60 m | 32 ft 6 in |
Length | 8.09 m | 27 ft 7 in |
Height | 3.33 m | 11 ft 11 in |
Wing area | 27.37 m2 | 294.61 sq ft |
PERFORMANCE |
Max. speed | 338 km/h | 210 mph |
Range | 917 km | 570 miles |
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