TEI-TF6000
Turbofan · Afterburning Turbofan
The TEI-TF6000 is an indigenous turbofan under development in the 6,000 lbf sea-level-static thrust class. The engine was run for the first time in February 2024. Designed to support an afterburning version, the TF6000 and derivatives of its core are intended for crewed and uncrewed aircraft as well as various land and maritime applications.
Key Features
- •6,000 lbf sea-level-static thrust
- •Design supporting an afterburning version
- •1.08 bypass ratio
- •Two-stage axial fan
- •Six-stage axial compressor
- •Single-stage high-pressure and low-pressure turbines
- •Variable-stator compressor
- •Mixed-flow exhaust
Example Platforms
No public information is available.
Source Notes
- •TEI identifies February 2024 as the first engine run but does not disclose the exact day.
- •An afterburner is not included in the current TF6000 technical-sheet thrust figure; the engine is designed to support an afterburning version.
- •No specific flight platform or first-flight date has been disclosed.