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J44

The Fairchild J44 was a small turbojet developed in the 1940s by the Fairchild Engine Division.

Design and development[edit | edit source]

The Fairchild Engine Division (previously the Ranger Aircraft Engine Division of the Fairchild Engine & Aircraft Corporation) began development of the J44 in 1947. It was used in target drones, missiles, and as jet boosters on several aircraft types.

Applications[edit | edit source]

Specifications[edit | edit source]

General characteristics
  • Type: turbojet
  • Length:
  • Diameter:
  • Dry weight: 363 lb. (165 kg.)
Components
  • Compressor: single stage centrifugal flow compressor
  • Combustors: annular combuster
  • Turbine: two-stage turbine
  • Fuel type: JP-4
Performance
  • Maximum thrust: 2450 lb. (10.9 kN)
  • Specific fuel consumption: 0.94 SFC
  • Thrust-to-weight ratio: 6.5:1


See also[edit | edit source]

References[edit | edit source]

  • The History of North American Small Gas Turbine Aircraft Engines, William Fleming and Richard Leyes, AIAA, 1999
  • Kay, Anthony L. (2007). Turbojet History and Development 1930-1960 Volume 2:USSR, USA, Japan, France, Canada, Sweden, Switzerland, Italy and Hungary (1st ed.). Ramsbury: The Crowood Press. ISBN 978-1861269393. 

External links[edit | edit source]

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