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North American NA-40

From Wikipedia, the free encyclopedia
American prototype bomber aircraft
NA-40
General information
TypeAttack bomber
National originUnited States
ManufacturerNorth American Aviation
Primary userUnited States Army Air Corps
Number built1
History
First flightJanuary 1939
Developed fromNorth American XB-21
Developed intoNorth American B-25 Mitchell

TheNorth American NA-40 was an American prototypebomber aircraft developed byNorth American Aviation in the late 1930s for evaluation by theUnited States Army Air Corps. Although unsuccessful, it led directly to theNorth American B-25 Mitchell medium bomber.

Design and development

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NA-40 prototype front view, showing constant dihedral wing discarded early in development of the successor B-25 design

The Air Corps issued a circular (number 38-385) in March 1938 describing the performance they required from the next bombers — a payload of 1,200 lb (540 kg) with a range of 1,200 mi (1,900 km) at more than 200 mph (320 km/h).[1] Several American aircraft companies responded with submissions: Bell Model 9 with two engines,Boeing-Stearman Model X-100 with Pratt & Whitney R-2180 radials,Douglas Model 7B with Pratt & Whitney R-1830 Twin Wasp radials,Martin Model 167F[1] and North American submitted their NA-40 design. The NA-40 had benefited from theNorth American XB-21 (NA-39) of 1936, which was the company's partly successful design for an earlier medium bomber that had been initially accepted and ordered, but then cancelled. However, the company's experience from the XB-21 contributed to the design and development of the NA-40. The single NA-40 built flew first at the end of January 1939. It went through several modifications to correct problems. These improvements included fitting 1,600 hp (1,193 kW)Wright R-2600 "Twin Cyclone"radial engines, in March 1939, which solved the lack of power.[1]

In March 1939, North American delivered the substantially redesigned and improved NA-40 (as NA-40B) to theUnited States Army Air Corps for evaluation.[1] It was in competition with other manufacturers' designs produced - the Bell had not been built - Douglas 7B, Stearman XA-21, and the Martin Model 167F[2] but failed to win orders. The aircraft was originally intended to be an attack bomber for export to the United Kingdom and France, both of which had a pressing requirement for such aircraft in the early stages of World War II.

Despite the loss of the 7B in an accident injuring a French observer in January, the French had ordered the 7B and a revised version (as the DB-7). Unfortunately, the NA-40B was destroyed in acrash on 11 April 1939 while undergoing testing. Although the crash was not considered due to a fault with the aircraft design, the U.S. Army ordered the DB-7 as theA-20 Havoc.[3][4]

The Air Corps issued a specification for a medium bomber in March 1939 that was capable of carrying a payload of 2,400 lb (1,100 kg) over 1,200 miles (1,900 km) at 300 mph (480 km/h)[5] NAA used the NA-40B design to develop the NA-62, which competed for the medium bomber contract. No YB-25 was available for prototype service tests. In September 1939, the Air Corps ordered the NA-62 into production as the B-25, along with the other new Air Corps medium bomber, theMartin B-26 Marauder "off the drawing board".

Variants

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North American NA-40B prototype side
NA-40
A twin-engined, five-seat bomber to meet 1938 USAAF requirement for an attack bomber, it was powered by two 1,100 hp (820 kW)Pratt & Whitney R-1830-56C3G radials. Wingspan was 66 ft (20.12 m), and length 48 ft 3 in (14.71 m). First flown on 29 January 1939, it proved to be underpowered and unstable.[6][7]
NA-40B
The NA-40B (also known as the NA-40-2) was a modification of the NA-40 prototype with two 1,600 hp (1,193 kW) Wright R-2600-A71-3 radials and numerous minor changes. It first flew in revised form on 1 March 1939, but crashed on 11 April 1940.[6]
NA-40-3 through NA-40-7
Proposed export versions, not built.[8]

Specifications (NA-40B)

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Data from Baugher[1]

General characteristics

  • Crew: 5
  • Length: 47 ft 10 in (14.58 m)
  • Wingspan: 66 ft (20 m)
  • Wing area: 559 sq ft (51.9 m2)
  • Empty weight: 13,961 lb (6,333 kg)
  • Gross weight: 19,741 lb (8,954 kg)
  • Powerplant: 2 ×Wright R-2600-A71-3 Twin Cyclone 14-cylinderradial engines, 1600 hp (1193 kW) each at take-off power atsea level, and 1275 hp (951 kW) each at 12,000 ft (3.6 km)

Performance

  • Maximum speed: 309 mph (497 km/h, 269 kn) at 14,000 ft (4,300 m)

Armament

  • Guns: 3x 0.30 in (7.6 mm) flexible machine guns (nose, turret and ventral/waist)
  • Bombs: designed for 2,100 lb (950 kg)

See also

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Related development

Aircraft of comparable role, configuration, and era

Related lists

References

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Notes

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  1. ^abcdeBaugher, Joe."North American NA-40."American Military Aircraft: US Bomber Aircraft, 6 March 2000. Retrieved: 24 May 2015.
  2. ^Baugher, Joe."Douglas Model 7B."American Military Aircraft: US Bomber Aircraft, 2000. Retrieved: 28 May 2015.
  3. ^Parker 2013, pp. 77–79, 83, 88, 92.
  4. ^Borth 1945, pp. 70, 92, 244.
  5. ^Baugher, Joe."North American B-25 Mitchell."American Military Aircraft: US Bomber Aircraft, 6 March 2000. Retrieved: 24 May 2015.
  6. ^abDorrWings of Fame Volume 3, p. 124.
  7. ^"North American".Aerofiles, 2009. Retrieved: 12 December 2011.
  8. ^McDowell, Ernest (1978).B-25 Mitchell In Action. Squadron/Signal Publications, Inc. p. 3.ISBN 0-89747-033-8.

Bibliography

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  • Borth, Christy.Masters of Mass Production. Indianapolis, Indiana: Bobbs-Merrill Co., 1945.
  • Donald, David, ed.The Complete Encyclopedia of World Aircraft. London: Orbis, 1997.ISBN 0-7607-0592-5.
  • Dorr, Robert F. "North American B-25 Variant Briefing".Wings of Fame, Volume 3, 1996. London: Aerospace Publishing.ISBN 1-874023-70-0.ISSN 1361-2034. pp. 118–141.
  • Jones, Lloyd S.U.S. Bombers, B1-B70. Fallbrook, California: Aero Publishers, 1962.ASIN B0007FFBSO.
  • Norton, Bill.American Bomber Aircraft Development in World War 2. Hersham, Surrey, UK: Midland Publishing, 2012.ISBN 978-1-85780-330-3.
  • Parker, Dana T.Building Victory: Aircraft Manufacturing in the Los Angeles Area in World War II. Cypress, California: Dana Parker Enterprises, 2013.ISBN 978-0-9897906-0-4.
  • Reuter, Claus.Development of Aircraft Turrets in the AAF, 1917–1944. New York: S.R. Research & Publishing, 2000.ISBN 1-894643-08-9.
  • Rusinek, Ed."A Tale of Two Dragons."North American Aviation Retirees Bulletin, Winter 2005.
  • Yenne, Bill.The American Aircraft Factory in World War II. St. Paul, Minnesota: Zenith Press, 2006.ISBN 0-7603-2300-3.

External links

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