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Teledyne CAE J700

From Wikipedia, the free encyclopedia
J700
Type Turbojet
National origin United States
Manufacturer Teledyne CAE
Major applications ADM-141 TALD

The Teledyne CAE J700 is a small turbojet engine designed to power unmanned air vehicles such as missiles. It was developed for and powers the ADM-141C ITALD air-launched decoy missile.

Design and development

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In the early 1990s, Brunswick developed an improved version of the ADM-141 TALD decoy missile with turbojet power, the ADM-141C. Teledyne CAE responded by developing the J700 turbojet for the ADM-141C, giving the missile improved range and a flight profile resembling aircraft.[1][2]

Variants

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J402-CA-100

Applications

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Specifications (J700-CA-400)

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Data from [1]

General characteristics

  • Type: Turbojet
  • Length:
  • Diameter:
  • Dry weight:

Components

  • Compressor:

Performance

  • Maximum thrust: 180 lbf (0.78 kN)

References

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  1. ^ a b Parsch, Andreas. "IMI (Brunswick) ADM-141 TALD". designation-systems.net. Retrieved 12 February 2019.
  2. ^ "Military Turbojet/Turbofan Specifications". jet-engine.net. Retrieved 12 February 2019.

Further reading

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  • Leyes, Richard A. II; William A. Fleming (1999). The History of North American Small Gas Turbine Aircraft Engines. Reston, VA: American Institute of Aeronautics and Astronautics. ISBN 1-56347-332-1.