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T- MET18SRC turbocharger rotor assembly belongs to one part of T- Mitsubishi / T- MET-SRC series exhaust gas turbocharger with the design features as below:
| T- MET | T- SRC Series | Engine Output (kW)* | Max. Pressure Ratio | L (mm) | W (mm) | H (mm) |
| T- MET18SRC | 400-1,100 | 5.5 | 712 | 510 | 510 | |
| T- MET22SRC | 650-1,600 | 5.5 | 835 | 605 | 605 | |
| T- MET26SRC | 850-2,200 | 5.5 | 1,075 | 735 | 735 | |
| T- MET30SRC | 1,150-3,300 | 5.5 | 1,368 | 860 | 860 | |
| T- MET37SRC | 2,200-4,400 | 5.5 | 1,661 | 1,070 | 1,070 |
Note: *Engine Output Range is for reference subject to pressure ratio 3.5.
The turbocharger rotor assembly / rotor complete consists of compressor impeller, blade shaft, turbo shaft and partition wall complete.
The compressor impeller is of aluminium alloy or the more expensive titanium. The turbocharger rotor shaft is equipped with components such as a compressor and a turbine impeller, and has a complicated structure and a large weight.