The extinction monitor developed under this program will significantly benefit the scientific community interested in characterizing the radiative propertes of ambient aerosols. The ability of one instrument to simultaneously measure particle extinction at one or more wavelengths with good time resolution and high precision will enable continuous measurements of the particle extinction that can be directly used by regional and global climate forcing models. The development of a CAPS-based extinction monitor would have the largest impact on the ambient air quality monitoring community. PM2.5 and PM10 levels must be routinely monitored as part of ambient air pollution monitoring programs and current technology is labor intensive and expensive.
The primary NASA need for this technology is in its programs to monitor particulate emissions from rocket and aircraft engines. The impact of particulate emissions from aircraft engines, which have a direct effect on radiative forcing, is magnified by the fact they are typically emitted in the upper troposphere and lower stratosphere where their influence is greatest. In addition, ground-based emissions of small particulates (i.e., PM10 and PM2.5) are regulated by the EPA. As aircraft engine soot emissions continue to decrease in response to regulations concerning the emission of species related to global warming and climate change as well as ground-based PM particulate emissions, the performance of commercially available instruments will become a hindrance to the accurate determination of such emissions.
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