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Aviation and the Global Atmosphere

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<strong>Aviation</strong> <strong>and</strong> <strong>the</strong> <strong>Global</strong> <strong>Atmosphere</strong><br />

<strong>Aviation</strong> <strong>and</strong> <strong>the</strong> <strong>Global</strong> <strong>Atmosphere</strong><br />

Table of contents | Previous page | Next page<br />

EXECUTIVE SUMMARY<br />

Although aircraft generally fly in corridors, <strong>the</strong>ir atmospheric effects are expected to propagate far beyond those regions.<br />

O<strong>the</strong>r reports in this collection<br />

For subsonic aircraft flying in <strong>the</strong> troposphere <strong>and</strong> <strong>the</strong> lowermost part of <strong>the</strong> stratosphere, emissions of oxides of nitrogen (NOx ) are <strong>the</strong> primary cause for <strong>the</strong> modelcalculated<br />

increase in ozone (O3 ) in <strong>the</strong> upper troposphere (UT). Emissions of NOx , water vapor (H2O), <strong>and</strong> sulfate from supersonic aircraft cruising in <strong>the</strong> stratosphere<br />

are expected to decrease <strong>the</strong> column abundance of O3 .<br />

The effects of aircraft emissions are strongly dependent on flight altitudes: Emissions in <strong>the</strong> troposphere <strong>and</strong> <strong>the</strong> stratosphere have distinctly different effects on O3 .<br />

Although <strong>the</strong> global chemical transport models used in this assessment attempt to simulate both <strong>the</strong> troposphere <strong>and</strong> <strong>the</strong> stratosphere, <strong>the</strong>se models have been<br />

developed for simulating ei<strong>the</strong>r <strong>the</strong> troposphere or <strong>the</strong> stratosphere, but not both. Thus, <strong>the</strong> assessment of O3 impact focuses on subsonic aircraft effects using<br />

tropospheric models <strong>and</strong> supersonic effects using stratospheric models. This approach is probably valid for supersonic aircraft, which cruise exclusively in <strong>the</strong><br />

stratosphere (19 km), but it may be problematic for subsonic aircraft that have a sizable amount of emissions in <strong>the</strong> lowest levels of <strong>the</strong> stratosphere (around 12 km at<br />

mid-latitudes). The impact of subsonic emissions on <strong>the</strong> stratosphere has not been fully evaluated using models <strong>and</strong> requires fur<strong>the</strong>r investigation.<br />

Calculations for Subsonic Aircraft Scenarios<br />

Model calculations were designed to assess <strong>the</strong> effects of added NO x . They concluded that <strong>the</strong>re would be an increase in ozone concentration <strong>and</strong> a decrease in<br />

methane (CH 4 ) concentration.<br />

NO x -All models compute increases of NO x in <strong>the</strong> upper troposphere (UT)/lower stratosphere (LS) of 50-150 pptv at 12 km at mid-latitudes for 2015; <strong>the</strong>se increases<br />

are significant compared to <strong>the</strong> average background levels of 50-200 pptv.<br />

http://www.ipcc.ch/ipccreports/sres/aviation/045.htm (1 von 4)08.05.2008 02:42:16

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