EJ200
A joint MTU, Rolls-Royce, Avio and ITP effort, the EJ200 is an advanced engine powering the Eurofighter and its export version Typhoon. It is a brand new two-shaft turbofan engine in the 90kN thrust category.
MTU's production share is 30% and comprises the low- and high-pressure compressors, electronic control unit, plus work on the high-pressure turbine as well as assembly and testing of the engines for the German air force.
| Technical Data | |
|---|---|
| Max. thrust with afterburner | 90 kN |
| Max. thrust without afterburner | 60 kN |
| Thrust-weight ratio | 10:1 |
| Fan pressure ratio | 4.2:1 |
| Bypass ratio | 0.4:1 |
| Pressure ratio | 26:1 |
| Air mass flow | 75-77 kg/s |
| Length incl. afterburner | 4000 mm |
| Max. inlet diameter | 740 mm |
| Weight incl. afterburner | 990-1035 kg |
Facts:
- Two-shaft turbofan engine with afterburner
- Blisk Low-pressure compressor and High-pressure compressor (Integrally bladed disk)
- Single-crystal turbine blades
- Convergent/divergent nozzle
- Modular design
- Digital control unit
- On-condition maintenance
Development and production:
- Low-pressure compressor
- High-pressure compressor
- Digital control unit (Digital Engine Control and Monitoring Unit DECMU)
- Final assembly of German engines
Support:
- Maintenance and repair of engines and modules under the "cooperative model" at MTU Aero Engines in Munich.
- Technical-logistic support
Application & Partners
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| Eurofighter |
MTU share: 33% development / 30% production
Partners:
- Rolls-Royce (Great Britain)
- Avio (Italy)
- ITP (Spain)

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