General Electric YJ101

YJ101
Type Turbofan
National origin United States
Manufacturer General Electric Aircraft Engines
First run 1978
Major applications Northrop YF-17
Developed into General Electric F404

The General Electric YJ101 was an afterburning turbofan engine in the 15,000 lbf class (static thrust). Developed for the Northrop YF-17 entry in the Lightweight Fighter (LWF) competition, the YJ101 formed the basis for General Electric's highly successful F404 engine.

Applications

Specifications (YJ101)

General characteristics

Components

Performance

See also

Related development


Related lists

References

    External links

    This article is issued from Wikipedia - version of the Wednesday, June 24, 2015. The text is available under the Creative Commons Attribution/Share Alike but additional terms may apply for the media files.