IAR K14

From Wikipedia, the free encyclopedia
Jump to: navigation, search
IAR K14
Piaggio-P.XI.jpg
Preserved Piaggio P.XI
Type Radial engine
National origin Romania
Manufacturer Industria Aeronautică Română
First run 1937
Major applications IAR 80, IAR 37, IAR 39
Number built 1000
Developed from Gnome-Rhône Mistral Major

The IAR K14 was a Romanian 14-cylinder radial aircraft engine. The IAR K14 was a licensed derivative of the French Gnome-Rhône Mistral Major 14K produced in Romania.[1]

Variants[edit]

Applications[edit]

Specifications[edit]

General characteristics

  • Type: Fourteen-cylinder two-row air-cooled radial engine
  • Bore: 146 mm (5.748 in)
  • Stroke: 165 mm (6.496 in)
  • Displacement: 38.673 l (2,360 in³)
  • Diameter: 1,296 mm (51.02 in)
  • Dry weight: 540 kg (1,190 lb)

Components

Performance

See also[edit]

Related development
Comparable engines
Related lists

References[edit]

Notes[edit]

  1. ^ Gunston 1989,

Bibliography[edit]

  • Gunston, Bill. World Encyclopedia of Aero Engines. Cambridge, England. Patrick Stephens Limited, 1989. ISBN 1-85260-163-9