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
- Type: Turbofan
- Length:
- Diameter:
- Dry weight:
Components
Performance
See also
- Related development
- Related lists
References
- Spick, Mike (2000). The Great Book of Modern Warplanes. Osceola, WI: MBI Publishing Company. ISBN 0-7603-0893-4.
External links
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