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Teledyne CAE F106

The Teledyne CAE F106 (company designation Model 472) was a small American turbofan engine developed to power cruise missiles.

F106
Type Turbofan
National origin United States
Manufacturer Teledyne CAE
Major applications LTV BGM-110

Development and design

The F106 engine was developed during the early 1970s to power the missiles being developed for the United States Navy's cruise missile competition. It powered the LTV YBGM-110 which lost the competition to the BGM-109 Tomahawk. While the F106 only powered the YBGM-110 prototype, either it or the Williams F107 could have powered either missile.[1] However, the Navy selected the F107 engine with the BGM-109 missile.

The F106 engine was also a competitor to power the AGM-86 ALCM cruise missile for the United States Air Force, but it likewise lost to the Williams F107 engine.[1][2]

Specifications (F106-CA-100)

Data from [1]

General characteristics

  • Type: Turbofan
  • Length:
  • Diameter:
  • Dry weight:

Components

  • Compressor:

Performance

See also

Related lists

References

  1. ^ a b c Fulton, Kenneth. Turbine Engines of the World: Teledyne CAE (USA). Flight International. 2 January 1975, Vol. 107, No. 3434. p. 26.
  2. ^ Fulton, Ken. "International Turbine Engine Directory: Teledyne CAE (USA). Flight International. 13 January 1979, Vol. 115, No. 3643. pp. 132-133.

teledyne, f106, f106, redirects, here, interceptor, convair, delta, dart, company, designation, model, small, american, turbofan, engine, developed, power, cruise, missiles, f106type, turbofannational, origin, united, statesmanufacturer, teledyne, caemajor, ap. F106 redirects here For the jet interceptor see Convair F 106 Delta Dart The Teledyne CAE F106 company designation Model 472 was a small American turbofan engine developed to power cruise missiles F106Type TurbofanNational origin United StatesManufacturer Teledyne CAEMajor applications LTV BGM 110 Contents 1 Development and design 2 Specifications F106 CA 100 2 1 General characteristics 2 2 Components 2 3 Performance 3 See also 4 ReferencesDevelopment and design EditThe F106 engine was developed during the early 1970s to power the missiles being developed for the United States Navy s cruise missile competition It powered the LTV YBGM 110 which lost the competition to the BGM 109 Tomahawk While the F106 only powered the YBGM 110 prototype either it or the Williams F107 could have powered either missile 1 However the Navy selected the F107 engine with the BGM 109 missile The F106 engine was also a competitor to power the AGM 86 ALCM cruise missile for the United States Air Force but it likewise lost to the Williams F107 engine 1 2 Specifications F106 CA 100 EditData from 1 General characteristics Type Turbofan Length Diameter Dry weight Components Compressor Performance Maximum thrust 614 lbf 2 7 kN Power to weight ratio See also EditRelated lists List of aircraft enginesReferences Edit a b c Fulton Kenneth Turbine Engines of the World Teledyne CAE USA Flight International 2 January 1975 Vol 107 No 3434 p 26 Fulton Ken International Turbine Engine Directory Teledyne CAE USA Flight International 13 January 1979 Vol 115 No 3643 pp 132 133 This aircraft engine article is missing some or all of its specifications If you have a source you can help Wikipedia by adding them Retrieved from https en wikipedia org w index php title Teledyne CAE F106 amp oldid 896084132, wikipedia, wiki, book, books, library,

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