Teledyne CAE J69

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J69 / J100
Teledyne-Continental J69.jpg
Teledyne-Continental J69 turbojet, Warner-Robbins Air Museum, Georgia
Type Turbojet
National origin France/United States
Manufacturer Continental Aviation and Engineering / Teledyne CAE
Major applications BQM-34 Firebee
T-37 Tweet
Developed from Turbomeca Marboré

The Teledyne CAE J69 was a small turbojet engine originally produced by Continental Aviation and Engineering (CAE) under license from Turbomeca. A development of the Turbomeca Marboré II, the J69 powered a number of US drones, missiles and small aircraft. Later produced by Teledyne CAE, the J69 was also developed into the Teledyne CAE J100 turbojet optimized for higher altitudes

Variants[edit]

J69
[1]
J69-T-9
J69-T-19B
J69-T-25
J69-T-27
J69-T-29
J69-T-31
J69-T-33
J69-T-41A
J100-CA-100
2,800 lbf (12 kN) thrust
CJ69-1025
1,025 lbf (4.56 kN)
CJ69-1400
1,400 lbf (6.2 kN) lb thrust
Model 352-5a
(CJ69-T-1025) 1,025 lbf (4.56 kN) thrust
Model 354-12
(J69-T-27) 1,150 lbf (5.1 kN) thrust
Model 356-7A
(J69-T-29) 17,005 lbf (75.64 kN) thrust
Model 356-7D
(J69-T-29) 1,700 lbf (7.6 kN) thrust
Model 356-8
(J69-T-31) 1,025 lbf (4.56 kN) thrust
Model 356-11
(J69-T-33) 1,025 lbf (4.56 kN) thrust
Model 356-29A
(J69-T-41A)

Applications[edit]

The J69 of a TT-1 Pinto
J69
J100

Specifications (Marboré IIC)[edit]

Data from FAA Type Certificate Data Sheet[2]

General characteristics

  • Type: Turbojet
  • Length: 61.7 in (156.7 cm)
  • Diameter: 24.9 in (63.2 cm)
  • Dry weight: 358 lb (162.4 kg)

Components

  • Compressor: Single stage centrifugal
  • Combustors: Single annular combustion chamber
  • Turbine: Single stage

Performance

See also[edit]

Related development
Related lists

References[edit]

  1. ^ Flying Magazine: 27. August 1961. 
  2. ^ FAA Type Certificate Data Sheet Retrieved: 2 November 2008
  • Gunston, Bill (2006). World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. p. 79. ISBN 0-7509-4479-X. 
  • Leyes II, Richard A.; William A. Fleming (1999). The History of North American Small Gas Turbine Aircraft Engines. Washington, DC: Smithsonian Institution. ISBN 1-56347-332-1. 

External links[edit]