Engineering:Teledyne CAE J700
From HandWiki
Short description: Turbojet engine
| 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
- Maximum thrust: 180 lbf (0.78 kN)
- Power-to-weight ratio:
References
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.
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