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In 1932, the Vought company, believing an export market
to exist for a single-seat fighter among its existing
customers for the two-seat Corsair observation aircraft
and reconnaissance-bomber (eg, V-65 and V-66), developed
the V-80. Designed to adhere structurally as
closely as possible to the two-seater to simplify spares
supply and maintenance, a V-80 demonstrator was
flown early in 1933. Powered by a Pratt & Whitney
R-1340-SD Hornet engine rated at 675hp at 1830m, the V-80 had provision for an armament of
four 7.62mm guns, two in the upper wing
centre section and two firing through the engine cowling,
and could carry a 227kg bomb load. The
standard wheel undercarriage was interchangeable
with a single central float with outrigger stabilising
floats. Three examples (V-80P) were ordered by Peru,
these having the 700hp R-1690-T1D1 Hornet and the
first example flew on 19 May 1933. These were supplied
with the interchangeable float undercarriages. One further example was built, the V-80F with a similarly-rated
R-1690-SD engine, this being flown on 10 April
1934 and sold to Argentina. The original V-80 demonstrator,
with armament removed, was sold as the V-135
to the. Connecticut State Department of Aeronautics,
and, in 1935, was utilised by Pratt & Whitney as an
engine test bed.
| MODEL | V-80P |
| WEIGHTS |
| Take-off weight | 2203 kg | 4857 lb |
| Empty weight | 1608 kg | 3545 lb |
| DIMENSIONS |
| Wingspan | 10.97 m | 35 ft 12 in |
| Length | 9.44 m | 30 ft 12 in |
| Height | 3.19 m | 10 ft 6 in |
| Wing area | 31.31 m2 | 337.02 sq ft |
| PERFORMANCE |
| Max. speed | 304 km/h | 189 mph |
| Range | 1233 km | 766 miles |
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