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Model 146
Martin Model 146
Martin Model 146 during competition c. 1935, USAF photo
Role Medium bomber
Manufacturer Glenn L. Martin Company
Designer Peyton M. Magruder
First flight 1935
Introduction 1934
Status Experimental prototype
Primary user United States Army Air Corps (intended)
Produced 1935
Number built 1
Variants Martin B-10

The Martin Model 146 was an unsuccessful American bomber design that lost to the Boeing Model 299 which spawned the famous B-17 Flying Fortress.

Design and development[]

Although generally satisfied with the speed and bombload of the Martin B-10, the United States Army Air Corps wanted a longer ranging bomber. Two competitions were held in 1934-35: one for fast bombers capable of flying 2,200 miles (3,500 km), and a second for the experimental prototype of a 5,000-mile (8,000 km) bomber.

The Martin 146 was built for the first competition, competing with the Boeing Model 299 (later the B-17) and Douglas DB-1 (later the B-18). The Model 146 bore a striking resemblance to the earlier Martin B-10, with the same configurations of turret and cockpits and even the same two Wright Cyclone engines – "hardly positive selling points for a customer looking for the latest technology". The biggest difference between this plane and the Martin 139 (B-10) was it was wider allowing the Pilot and Copilot to sit side by side.[1]

The Model 146 was not successful but it led the Martin company to begin research into contemporary aviation technology. Some offshoots included the innovative Model 145 proposed for the long range bomber competition as well as the early studies that would lead to the Model 179 (later to emerge as the wartime Martin B-26). The final disposition of the Model 146 is currently not known.

Specifications (Model 146)[]

General characteristics

  • Crew: 4
  • Length: 52 ft 0 in (15.5 m)
  • Wingspan: 75 ft 1 in (22.9 m)
  • Height: 15 ft 5 in (4.7 m)
  • Wing area: 729 ft² (67.7 m²)
  • Loaded weight: 16,000 lb (7,257 kg)
  • Max. takeoff weight: 17,100 lb (7,756 kg)
  • Powerplant: 2 × Wright R-1820-G5 Cyclones "Cyclone" radials, 800 hp (597 kW) each

Performance

  • Maximum speed: 234 mph (203 knots, 377 km/h)
  • Cruise speed: 204 mph (177 knots, 328 km/h)
  • Range: 1,237 mi (1,075 nmi, 1,991km)
  • Service ceiling: 28,500 ft (8,687 m)
  • Wing loading: 21.95 lb/ft² (107.2 kg/m²)
  • Power/mass: 0.100 hp/lb (164.5 W/kg)

Armament

[2]

See also[]

References[]

Notes
  1. "Model 146." marylandaviationmuseum.org. Retrieved: 5 December 2o12.
  2. Martin 146 Specifications.' marylandaviationmuseum.org. Retrieved: 5 December 2012.
Bibliography
  • Baugher, Joe. "Martin B-10". Encyclopedia of American Aircraft. Retrieved: 4 July 2007.
  • Taylor, John W. R. "Martin B-10". Combat Aircraft of the World from 1909 to the Present. New York: G.P. Putnam's Sons, 1969. ISBN 0-425-03633-2.

External links[]

All or a portion of this article consists of text from Wikipedia, and is therefore Creative Commons Licensed under GFDL.
The original article can be found at Martin 146 and the edit history here.
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