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Deleted member 5
| TYPE | Research & Development |
| COUNTRY | Taiwan |
| PROJECT | AIDC TIG-05 |
| PROJECT COST | 15,000,000.00 |
| COMPLETION DATE | 24/09/2018 |
| PROJECT INFORMATION | The AIDC TIG-05 is a low bypass afterburning turbofan jet engine being developed in a joint venture between the Taiwanese companies AIDC and NCSIST in order to provide the upcoming air force fighter and strike aircraft program with an efficient, reliable and powerful indigenous supersonic engine. The TIG-05 is aimed to produce up to 159 kN (35744 lbf) thrust. [General Specification:] Length: 350 cm Diameter: 75 cm Dry weight: 2400 kg [Components:] Compressor: Twin-spool non-afterburning turbofan Overall Pressure Ratio: 18:1 Combustors: Can-type Turbine: 2 stage high pressure turbine, 4 stage low pressure turbine [Performance:] Maximum thrust: 159 kN (35744 lbf) with afterburner |
| PRIVATE / ENCRYPTED | Yes |
