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[]

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[]

J402-CA-100
  • Variant of the engine used in the ADM-141C ITALD.

Applications[]

  • ADM-141C ITALD

Specifications (J700-CA-400)[]

Data from [1]

General characteristics

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

Components

  • Compressor:

Performance

References[]

  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[]

  • 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.
Retrieved from ""