TEI-TF10000
Turbofan · Afterburning Turbofan
The TEI-TF10000 is an indigenous turbofan under development with a stated dry thrust of 6,000 lbf and afterburning thrust of 10,000 lbf. TEI envisages the engine powering a range of crewed and uncrewed aviation platforms while contributing technology toward a future engine for KAAN.
Key Features
- •Target afterburning thrust of 10,000 lbf
- •6,000 lbf dry thrust
- •1.08 bypass ratio
- •Two-stage axial fan
- •Six-stage axial compressor
- •Single-stage high-pressure and low-pressure turbines
- •Variable-vane mechanism
- •Turbine-cooling technology
Example Platforms
No public information is available.
Source Notes
- •TEI's sources do not disclose a specific flight platform, first engine test, first-flight date, dry weight, fuel type or maintenance interval.
- •The thrust figures are stated by the manufacturer for sea-level-static ISA conditions.