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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 />

heterogeneous reaction between ozone <strong>and</strong> soot proceeds at <strong>the</strong> highest reported rate (<strong>the</strong> one used in <strong>the</strong><br />

Bekki calculation), namely g(O3 ) = 3.0 x 10-4 (Stephens et al., 1986; Fendel et al., 1995; Rogaski et al.,<br />

1997), <strong>the</strong> time required to consume <strong>the</strong> mass of soot present in <strong>the</strong> stratosphere would be approximately 10<br />

minutes. It is important to note that this result is independent of <strong>the</strong> soot surface-to-volume ratio; it depends<br />

only upon <strong>the</strong> ozone concentration, which is taken to be 1011 cm-3 at 10-km altitude. At this reaction rate,<br />

only 5 hours would be required to consume <strong>the</strong> entire soot particulate population at 10 km (assuming 5 x 107<br />

carbon atoms cm-3 at a soot loading of 1 ng m-3 ) <strong>and</strong> cause <strong>the</strong> effective soot-ozone reaction rate to drop to<br />

zero.<br />

Laboratory evidence suggests that <strong>the</strong> soot-ozone reaction rate decreases after consumption <strong>and</strong> alteration<br />

of <strong>the</strong> top surface carbon layer (Stephens et al., 1986). Small reported laboratory g values-on <strong>the</strong> order of 3.0<br />

x 10 -5 -likely reflect <strong>the</strong> reaction rate associated with a "deactivated" laboratory soot surface. Using this value<br />

for g, <strong>the</strong> time required to consume individual particles of soot would be less than a day, <strong>and</strong> <strong>the</strong> time to<br />

consume all atmospheric soot would be leng<strong>the</strong>ned to approximately 3 weeks. Although this change in<br />

reaction rate extends <strong>the</strong> lifetime of atmospheric soot, it comes at <strong>the</strong> expense of <strong>the</strong> overall ozone<br />

destruction rate. Accordingly, our analysis indicates that <strong>the</strong> massof soot in <strong>the</strong> UT <strong>and</strong> LS does not seem to<br />

be sufficient to quantitatively affect ozone, regardless of <strong>the</strong> reaction rate chosen.<br />

In support of this conclusion, we note that in situ measurements in <strong>the</strong> engine exhaust of a Concorde<br />

supersonic aircraft in <strong>the</strong> LS have been used recently to constrain heterogeneous reaction rates on soot<br />

particles in a plume model (Gao et al., 1998). Gao et al. inferred low reactivity for <strong>the</strong> ozone-soot interaction;<br />

coupled with <strong>the</strong> measured abundance of <strong>the</strong> soot aerosol, Gao et al. reach <strong>the</strong> same conclusion that we<br />

derived from our qualititative arguments. In summary, <strong>the</strong> few model calculations performed suggest that<br />

subsonic aircraft sulfate <strong>and</strong> soot emissions in <strong>the</strong> stratosphere act as substrates for ozone depletion. The<br />

magnitude of <strong>the</strong> depletions is likely to be small relative to ozone increases from NO x emissions, but <strong>the</strong><br />

depletions are highly uncertain because of <strong>the</strong> poorstate of underst<strong>and</strong>ing <strong>and</strong> model development relative to<br />

aerosol chemistry.<br />

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

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

http://www.ipcc.ch/ipccreports/sres/aviation/026.htm (6 von 6)08.05.2008 02:41:43<br />

Figure 2-5: Annual trends for <strong>the</strong> periods 1970-96<br />

<strong>and</strong> 1980-96 shown by ozonesonde measurements<br />

at Hohenpeissenberg, Germany. 95% confidence<br />

limits are shown [adapted from WMO (1998) by J.<br />

Logan].<br />

IPCC Homepage

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