Teledyne CAE J69


The Teledyne CAE J69 was a small turbojet engine originally produced by Continental Aviation and Engineering 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: 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: thrust
;Model 354-12: thrust
;Model 356-7A: thrust
;Model 356-7D: thrust
;Model 356-8: thrust
;Model 356-11: thrust
;Model 356-16:
;Model 356-24:
;Model 356-27B:
;Model 356-29A:

Applications

;J69
;J100