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Teledyne CAE J69

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

Variants

Data from: Aircraft engines of the World 1957

J69-T-1: (Marboré I) at 23,000 rpm.
J69-T-3: at 22,500 rpm for take-off.
J69-T-6:
J69-T-9:
J69-T-17:
J69-T-19:
J69-T-19A:
J69-T-19B:
J69-T-23:
J69-T-25:
J69-T-27:
J69-T-29:
J69-T-31:
J69-T-33:
J69-T-39:
J69-T-41:
J69-T-41A:
J69-T-406:
J100-CA-100: thrust
CJ69-1025:
CJ69-1400: lb thrust
Model 352:
Model 352A:
Model 352-5a: (CJ69-T-1025) thrust
Model 354-12: (J69-T-27) thrust
Model 356-7A: (J69-T-29) thrust
Model 356-7D: (J69-T-29) thrust
Model 356-8: (J69-T-31) thrust
Model 356-11: (J69-T-33) thrust
Model 356-16:
Model 356-24:
Model 356-27B:
Model 356-29A: (J69-T-41A)

Applications

J69
J100

Specifications (Marboré IIC)

See also

References

External links