Teledyne CAE J700

{{short description|Turbojet engine}}

{{Infobox Aircraft Begin

| name=J700

| image=

| caption=

}}{{Infobox Aircraft Engine

|type=Turbojet

|manufacturer=Teledyne CAE

|national origin=United States

|first run=

|major applications=ADM-141 TALD

|produced=

|number built=

|program cost=

|unit cost=

|developed from=

|variants with their own articles=

}}

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.{{cite web |last1=Parsch |first1=Andreas |title=IMI (Brunswick) ADM-141 TALD |url=http://www.designation-systems.net/dusrm/m-141.html |website=designation-systems.net |access-date=12 February 2019}}{{cite web |title=Military Turbojet/Turbofan Specifications |url=http://jet-engine.net/miltfspec.html |website=jet-engine.net |access-date=12 February 2019}}

Variants

;J402-CA-100

Applications

Specifications (J700-CA-400)

{{jetspecs

|ref=

|type=Turbojet

|length=

|diameter=

|weight=

|compressor=

|combustion=

|turbine=

|fueltype=

|oilsystem=

|power=

|thrust={{cvt|0.78|kN|lbf|order=flip}}

|compression=

|bypass=

|aircon=

|turbinetemp=

|fuelcon=

|specfuelcon=

|power/weight=

|thrust/weight=

}}

References

{{Reflist}}

=Further reading=

  • {{cite book

|title=The History of North American Small Gas Turbine Aircraft Engines

|last=Leyes

|first=Richard A. II

|author2=William A. Fleming

|year=1999

|publisher=American Institute of Aeronautics and Astronautics

|location=Reston, VA

|isbn=1-56347-332-1

}}

{{CAE/TTE aeroengines}}

{{USAF gas turbine engines}}

Category:1990s turbojet engines

J700

Category:Centrifugal-flow turbojet engines