Northrop XFT
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The Northrop XFT was an American prototype fighter aircraft of the 1930s. A single engined low-winged
monoplane A monoplane is a fixed-wing aircraft configuration with a single mainplane, in contrast to a biplane or other types of multiplanes, which have multiple planes. A monoplane has inherently the highest efficiency and lowest drag of any wing con ...
, it was designed and built to meet a
United States Navy The United States Navy (USN) is the maritime service branch of the United States Armed Forces and one of the eight uniformed services of the United States. It is the largest and most powerful navy in the world, with the estimated tonnage ...
order for an advanced carrier based fighter. It exhibited poor handling, and was rejected by the Navy, the single prototype being lost in a crash. A variant, the Northrop 3A, also was unsuccessful.


Development and design

In the early 1930s, the
United States Navy The United States Navy (USN) is the maritime service branch of the United States Armed Forces and one of the eight uniformed services of the United States. It is the largest and most powerful navy in the world, with the estimated tonnage ...
was interested in investigating the use of modern,
monoplane A monoplane is a fixed-wing aircraft configuration with a single mainplane, in contrast to a biplane or other types of multiplanes, which have multiple planes. A monoplane has inherently the highest efficiency and lowest drag of any wing con ...
s as fighter aircraft to replace the biplanes that equipped its fighter squadrons. In December 1932, it ordered the XF7B from
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, and based on the impressive performance of Northrop's Gamma and
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, both
stressed skin In mechanical engineering, stressed skin is a type of rigid construction, intermediate between monocoque and a rigid frame with a non-loaded covering. A stressed skin structure has its compression-taking elements localized and its tension-taking ...
monoplanes, placed an order with Northrop on May 8, 1933 for a single prototype fighter, designated XFT-1.Green and Swanborough 1994, pp.454-455.Francillion 1979, p.173. The resulting aircraft, which was designed by a team led by
Ed Heinemann Edward Henry Heinemann (March 14, 1908 – November 26, 1991) was a military aircraft designer for the Douglas Aircraft Company. Biography Heinemann was born in Saginaw, Michigan. He moved to California as a boy and was raised in Los Angeles. A ...
resembled a scaled-down Northrop Delta. It was a low-winged monoplane, of all-metal stressed skin construction. It had a fixed
tailwheel undercarriage Conventional landing gear, or tailwheel-type landing gear, is an aircraft undercarriage consisting of two main wheels forward of the center of gravity and a small wheel or skid to support the tail.Crane, Dale: ''Dictionary of Aeronautical Term ...
with its main gear fitted with streamlining trouser fairings. The pilot sat in an enclosed cockpit with a sliding canopy. It was powered by a single Wright R-1510
radial engine The radial engine is a reciprocating type internal combustion engine configuration in which the cylinders "radiate" outward from a central crankcase like the spokes of a wheel. It resembles a stylized star when viewed from the front, and is ...
. The XFT-1 first flew on January 16, 1934, being delivered to NAS Anacostia for evaluation by the Navy. While it was the fastest fighter yet tested by the U.S. Navy, its handling characteristics were poor. Although it was fitted with flaps to lower its landing speed, it was difficult to control at low speeds, and had poor forward visibility, major problems for an aircraft intended to operate off aircraft carriers. Its most serious problem, however, was its behavior when spinning, where the tail was subject to severe buffeting. In February 1934, test pilot
Vance Breese Vance Breese (1904–1973) was an American aviation engineer and test pilot. Early years Vance Breese was born in Keystone, Washington, on April 20, 1904. His education, in his own words was: "various engineering extension courses." More than an ...
landed the prototype XFT-1 without authorization at Glendale California at a Curtiss Wright Technical Institute location, and pictures of the XFT-1 were leaked to Janes AWA. It was fitted with a more powerful R-1510 engine in August 1934, but this did not improve performance, and it was returned to Northrop for more major modifications, being fitted with larger tail surfaces and a
Pratt & Whitney R-1535 The Pratt & Whitney R-1535 Twin Wasp Junior was an engine used in American aircraft in the 1930s. The engine was introduced in 1932 as a 14-cylinder version of the 9-cylinder R-985. It was a two-row, air-cooled radial design. Displacement was ...
Twin Wasp Junior
radial engine The radial engine is a reciprocating type internal combustion engine configuration in which the cylinders "radiate" outward from a central crankcase like the spokes of a wheel. It resembles a stylized star when viewed from the front, and is ...
, being redesignated XFT-2.Francillion 1979, pp.174-175. The XFT-2 was redelivered to Anacostia in April 1936,Francillion 1979, p.175. where it was found that while its performance had only slightly improved, its handling was even poorer than before, and it was rejected by the U.S. Navy as unairworthy. It was ordered to be returned to Northrop, and ignoring instructions to ship the aircraft back to Northrop's El Segundo factory, a test pilot attempted to fly the XFT-2 back to California, the aircraft entering a spin and crashing when crossing the
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on July 21, 1936. The design formed the basis of the Northrop 3A, almost identical to the XFT except for a retractable undercarriage, which first flew in 1935. It was another failure, having a tendency for unintentional spins. After the 3A and its
test pilot A test pilot is an aircraft pilot with additional training to fly and evaluate experimental, newly produced and modified aircraft with specific maneuvers, known as flight test techniques.Stinton, Darrol. ''Flying Qualities and Flight Testin ...
,
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Frank Scare, disappeared without trace on a flight over the
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off
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on 30 July 1935, Northrop abandoned the 3A project and sold its
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s to Chance Vought Aviation, where it became the
Vought V-141 The Vought V-141 (which was later redesignated V-143 after modification) was a prototype American single-seat fighter aircraft of the 1930s. It was a development of the unsuccessful Northrop 3-A design, but was itself a failure, being rejected ...
.Green and Swanborough 1994, p. 455.Angelucci and Bowers 1987, p. 361.


Variants

;XFT-1 :Initial prototype of this naval fighter powered by a Wright Whirlwind radial. ;XFT-2 :redesignated as the XFT-2 after some major modifications and fitting of a Pratt & Whitney R-1535 Twin Wasp Junior. ;Northrop 3A :Further development of the FT as a land-based fighter, almost identical to the XFT except for retractable undercarriage. ; Vought V-143 :Development by Vought after the purchase of the Northrop 3A design. ;Vought V-150 :The V-143 fitted with a R-1535. ;Vought AXV : Imperial Japanese Navy Air Service designation of the V-143 evaluated in Japan.


Specifications (XFT-1)


See also


References

*Angelucci, Enzo and Peter M. Bowers. ''The American Fighter: The Definitive Guide to American Fighter Aircraft From 1917 to the Present'', New York: Orion Books, 1987, . *Francillion, René J. ''McDonnell Douglas Aircraft since 1920''. London:Putnam, 1979. . *Green, William and Swanborough, Gordon. ''The Complete Book of Fighters''. New York: Smithmark, 1994. .


External links


Northrop XFT-1
''Flight''. {{USN fighters F01T 1930s United States fighter aircraft Single-engined tractor aircraft Low-wing aircraft