Pyrometry can be applied to high-temperature low-pressure gases with solids or liquids entrained, or gases at a high enough pressure to radiate in a continuum[1]. SpectroPyrometry has been applied to various plasmas and flames with success.
SpectroPyrometers report both tolerance and signal strength[2] with temperature. The graph below shows the temperature and signal strength for a rocket burn of around 0.8 seconds duration.
The constancy of temperature and signal strength are notable. Over three successive burns of the same engine, the temperature averaged 2740.7°C with a standard deviation of 1.8°C. The SpectroPyrometer's tolerance for the three burns averaged 15.2°C for an on-line accuracy of 0.5%. It should be noted that if conventional pyrometry were to be applied to rocket plumes, the result would depend on estimates of the emissivity of the plume. For these measurements, the SpectroPyrometer determined the values of emissivity in real time. For this measurement setup, the Signal Strength is exactly equal to the emissivity. Interestingly, the measured temperatures agreed with the theoretical predictions.
The graph below presents the same temperature data with Signal Strength (emissivity) on the right side y-axis.
The data indicate that the Signal Strength increases with power. The Signal Strength here is the product of the emissivity of the radiating material in the plasma stream and its density in the stream. Thus, for a given location (and temperature), it is seen that there is more material in the plasma stream for a higher power setting, which is the expected result. Further, it appears that the Signal Strength is relatively invariant with distance until the very farthest distance from the generator ("5"). This can be interpreted to give information about the emissivity of the material with temperature and about the spreading of the plasma beam with distance. (That is, the fixed optics of the FMPI SpectroPyrometer always subtend the same solid angle. Therefore, a decrease of emissivity implies a decrease of density of material in the field of view; i.e. the beam is spreading.)
The Spectral Signal Strength (Spectral Emissivity) was examined for the data generating the graphs above (the SpectroPyrometer is capable of presenting spectral signal strength/emissivity graphs on line and storing them to non-volatile memory). One such graph is reproduced below.
Note that the Signal Strength (Emissivity) is not constant with wavelength, i.e., not "gray". Conventional pyrometry would be unable to measure the temperature of this material for two reasons: the absolute value of emissivity changes with power setting, and the relative value of emissivity changes with wavelength. The last feature, the non-grayness, was unknown prior to the SpectroPyrometer's measurement. Further, the non-grayness is not a static variable of the material, but a dynamic variable of the application; it, too, can change during the deposition. The non-grayness, routinely found in metals, has been recorded by the SpectroPyrometer to vary around 10% for this process. The obvious conclusion is that only a pyrometer such as the SpectroPyrometer which is independent of emissivity's variations can measure temperature accurately for these materials.