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Computerized Micro Jet Engine Test Facility - Turbo & Jet Engine ...

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• Single spool<br />

• Radial compressor<br />

• Axial turbine<br />

• Pressure ratio: 4:1<br />

• Max. RPM: 108,000<br />

• Compressed air start‐up<br />

• Propane gas pre‐heating<br />

• Evaporators<br />

9 th Israeli Symposium on<br />

<strong>Jet</strong> <strong>Engine</strong>s and Gas<br />

Turbines,<br />

October 7 2010,<br />

Technion, Istarel<br />

AMT Olympus engine<br />

7<br />

<strong>Turbo</strong> and <strong>Jet</strong> <strong>Engine</strong><br />

Laboratory<br />

Technion –Israel<br />

www. jet‐engine‐lab.technion.ac.il

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