Trisha Shetty (Editor)

Teledyne CAE J69

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Teledyne CAE J69

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

Contents

Variants

J69
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

J69
  • Avro Canada VZ-9 Avrocar
  • Cessna T-37 Tweet
  • Radioplane Q-1
  • Ryan BQM-34 Firebee
  • Temco TT Pinto
    • J100
  • Ryan Model 147T

    • Specifications (Marboré IIC)

    Data from FAA Type Certificate Data Sheet

    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

  • Maximum thrust: 880 lbf (3.91 kN) at 22,600 rpm
  • Turbine inlet temperature: 650 C
  • Thrust-to-weight ratio: 2.458 lbf/lb (0.024 kN/kg)

    • References

    Teledyne CAE J69 Wikipedia
    (Text) CC BY-SA