Figure 8: Cut-away of the SR-30 engine Sensor Identification P01 Compressor stage static pressure. T01 Compressor inlet static temperature. – – P02 Compressor stage stagnation pressure. T02 Compressor stage exit stagnation – – temperature. P03 Combustion chamber pressure. T03 Turbine stage inlet stagnation – – temperature. P04 Turbine exit stagnation pressure. T04 Turbine stage exit stagnation – – temperature. P05 Thrust nozzle exit stagnation pressure. T05 Thrust nozzle exit stagnation   temperature.
Figure 8: Cut-away of the SR-30 engine Sensor Identification P01 – Compressor stage static pressure. T01 – Compressor inlet static temperature. P02 – Compressor stage stagnation pressure. T02 – Compressor stage exit stagnation temperature. P03 – Combustion chamber pressure. T03 – Turbine stage inlet stagnation temperature. P04 – Turbine exit stagnation pressure. T04 – Turbine stage exit stagnation temperature. P05  Thrust nozzle exit stagnation pressure. T05  Thrust nozzle exit stagnation temperature.