IAR K14

IAR K14
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

IAR K14-I 40
IAR K14-I C32
693 kW (930 hp) engine. 44 for IAR P.24E
IAR K14-II C32
649 kW (870 hp) engine. 50 built for IAR 37, 1 built for IAR 80 prototype
IAR K14-II D32
IAR K14-III C36
690 kW (930 hp) engine. 20 built for IAR 80, 95 built for IAR 37
IAR K14-IV C32
716 kW (960 hp) engine. 30 built for IAR 80, 160 built for IAR 39, 2 built for IAR 47 prototypes
IAR K14-IV C32 1000A
764 kW (1025 hp) engine. 430 built for IAR 80A,IAR 80B,IAR 80C, IAR 81A,IAR 81B,IAR 81C

Applications

Specifications

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

Related development

Comparable engines

Related lists

References

Notes

  1. ↑ Gunston 1989,

Bibliography

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