Northrop Gamma

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Northrop Gamma
Northrop Gamma 2A NR-12265 (16537176044) .jpg
Northrop Gamma
Type: Cargo plane
Design country:

United StatesUnited States United States

Manufacturer:

Northrop Aircraft Corporation

First flight:

1932

Number of pieces:

60

The Northrop Gamma was a single-engine, low- wing cargo aircraft made by the American Northrop Aircraft Corporation in the early 1930s.

history

In 1928 John Knudsen Northrop , the previous chief designer of Lockheed , founded the Avion Corporation (since 1929 part of the United Aircraft Corporation as Northrop Aircraft Corporation ) in Burbank , California . Based on the Lockheed Sirius he developed together with Jerry Vultee , in 1930 he designed the Northrop Alpha , which was improved in many details and designed as an all-metal aircraft , from which the Northrop Gamma was then developed. The first flight of the prototype took place in 1932.

construction

The hull of the cantilevered low- wing aircraft was constructed in half-shell construction. The aircraft had a rigid tail wheel landing gear .

A radial engine from Pratt & Whitney or Curtiss-Wright served as the drive .

Technical specifications

Parameter Data
crew 2
length 31 '2 "(9.50 m)
span 47 '9 1/2 "(14.57 m)
height 9 '(2.74 m)
Empty mass 4,100 lb (approximately 1,860 kg)
Max. Takeoff mass 7,350 lb (approx. 3,330 kg)
Cruising speed 222 mph (approx. 360 km / h) at 16,500 ft (approx. 5,000 m)
Top speed 228 mph (approx. 370 km / h) at 11,000 ft (approx. 3,400 m)
Service ceiling 25,600 ft (approx. 7,800 m)
Range 1,760 mi (approx. 2,830 km)
Engine Wright Cyclone with 750 PS (approx. 550 kW) in 11,000 ft (approx. 3,400 m)

See also

Web links

Commons : Northrop Gamma  - collection of images, videos, and audio files

Individual evidence

  1. Specification of American Airplanes. In: Aviation. McGraw-Hill Publishing Company, Inc., March 1936, pp. 33, 82-83 , accessed August 9, 2018 .