Teledyne CAE J69

J69 / J100
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

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

The J69 of a TT-1 Pinto
J69
J100

Specifications (Marboré IIC)

Data from FAA Type Certificate Data Sheet[2]

General characteristics

Components

Performance

See also

Related development

Related lists

References

  1. Flying Magazine: 27. August 1961. Missing or empty |title= (help)
  2. FAA Type Certificate Data Sheet Retrieved: 2 November 2008
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