Curtiss XF13C

XF13C
Curtiss XF13C in 1937
Role	Fighter
National origin	United States
Manufacturer	Curtiss Aeroplane and Motor Company
First flight	7 January 1934[1]

The Curtis XF13C (Model 70) was a carrier-based biplane fighter aircraft built by Curtiss Aeroplane and Motor Company.

Development and design

The XF13C was a naval fighter featuring an all-metal construction, with a semi-monocoque fuselage, manually retractable landing gear and an enclosed cockpit. The aircraft was designed to facilitate conversions from biplane to monoplane and vice-versa. The United States Navy bought a prototype, designated XF13C-1 when in monoplane configuration, and XF13C-2 when a biplane.^[1]

The XF13C first flew in 1934 with good results realized in tests. In 1935, the aircraft received a more powerful engine and modifications to the overly tall tailplanes. The designation was changed to XF13C-3 for more flight testing.

Operational history

No production orders were received for the Curtis XF13C, but the aircraft continued to fly for NACA in experimental work, and by VWJ-1 Squadron at Quantico.^[1]

Specifications (XF13C-3)

Data from ^[1]

General characteristics

• Crew: 1
• Length: 25 ft 0 in (7.62 m)
• Wingspan: 35 ft 0 in (10.66 m)
• Height: 8 ft 9.5 in (2.66 m)
• Wing area: 205 ft² (19.04 m²)
• Empty weight: 3.412 lb (1,548 kg)
• Gross weight: 4,634 lb (2,102 kg)
• Powerplant: 1 × Wright SGR-1510-12, 700 hp ( kW) each

Performance

• Maximum speed: 246 mph (396 km/h)
• Range: 726 miles (1,168 km)
• Service ceiling: 25,250 ft (7,696 m)
• Rate of climb: 2000 ft/min (10.16 m/s)

Armament

• 1 × .50 in (12.7 mm) machine gun
• 1 × .30 in (7.62 mm) machine gun

References

Notes

1. ^ ^{a b c d} Angelucci 1987, pp. 152–153.

Bibliography

• Angelucci, Enzo. The American Fighter from 1917 to the present. New York: Orion Books, 1987. ISBN 0-517-56588-9.