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SR30 Turbojet Engine


Specifications:

• Engine must utilize a centrifugal flow compressor, reverse flow annular combustor and an axial flow turbine stage.
• Operator capable of manual control throughout entire range of operation.
• Operator panel to consist of digital TIT, EGT, and RPM indicators, analog oil pressure, engine pressure ratio, fuel pressure and air pressure gauges, keyed master, green start, red stop and T-handled power control lever.
• System to be equipped with calibrated transducers and thermocouples capable of measuring compressor inlet, compressor exit, turbine stage inlet, turbine stage exit and thrust nozzle exit temperature and pressures, fuel flow, thrust and engine compressor / turbine rotational speed.

 View Datasheet

    Specifications:

    • Engine must utilize a centrifugal flow compressor, reverse flow annular combustor and an axial flow turbine stage.
    • Operator capable of manual control throughout entire range of operation.
    • Operator panel to consist of digital TIT, EGT, and RPM indicators, analog oil pressure, engine pressure ratio, fuel pressure and air pressure gauges, keyed master, green start, red stop and T-handled power control lever.
    • System to be equipped with calibrated transducers and thermocouples capable of measuring compressor inlet, compressor exit, turbine stage inlet, turbine stage exit and thrust nozzle exit temperature and pressures, fuel flow, thrust and engine compressor / turbine rotational speed.

     View Datasheet

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