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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 />

total fossil carbon emissions for a similar economic scenario (IS92a). Note <strong>the</strong> logarithmic scale<br />

in Figure 6-6. For scenario F1a, fuel use parallels that of IS92a, but for Eab it grows faster than<br />

total fossil fuel use. In converting aviation fuel to CO 2 emissions, we adopt a carbon fraction by<br />

weight of 86%. <strong>Aviation</strong> fuel use prior to 1992 is based on International Energy Agency data<br />

(IEA, 1991; for table, see Sausen <strong>and</strong> Schumann, 1999). To account for systematic<br />

underestimation of fuel use (see Chapter 9), we have increased NASA-1992 <strong>and</strong> NASA-2015<br />

emissions by 15% <strong>and</strong> 5%, respectively, to form <strong>the</strong> inventories NASA-1992* <strong>and</strong> NASA-2015*.<br />

Figure 6-7 gives an exp<strong>and</strong>ed linear scale of aviation fuel use from 1990 to 2050 for scenarios<br />

Fc1, Fa1, Fa1H, Fe1, Eab, <strong>and</strong> Edh, in order of increasing fuel use by 2050.<br />

Chapter 4 studies <strong>the</strong> impact of a fleet of high-speed civil transport (HSCT, i.e., supersonic)<br />

aircraft using a range of 3-D emission scenarios with atmospheric chemistry models. These<br />

calculations form a parametric range that covers changes in fleet size, NO x emissions, cruise<br />

altitude, sulfate aerosol formation, <strong>and</strong> future atmospheres. The present chapter combines those<br />

results into a continuous scenario for <strong>the</strong> HSCT fleet, designated Fa1H: On top of <strong>the</strong> Fa1<br />

scenario it assumes that HSCT aircraft come into service in 2015, grow at 40 planes per year to<br />

a final capacity of 1,000 aircraft by 2040, continue operation to 2050, <strong>and</strong> displace equivalent air<br />

traffic from <strong>the</strong> subsonic fleet (~11% of Fa1 in 2050). This Mach 2.4 HSCT fleet cruises at 18-20<br />

km altitude <strong>and</strong> deposits most of its emissions in <strong>the</strong> stratosphere. It has new combustor<br />

technology that produces very low emissions of 5 g NO2 per kg fuel. Table 6-1 gives <strong>the</strong><br />

breakdown of RF from two specific HSCT studies in Chapter 4: 500 HSCTs in a 2015<br />

background atmosphere <strong>and</strong> 1,000 HSCTs in a 2050 background atmosphere (e.g., chlorine<br />

loading, methane, nitrous oxide). The likely interval for <strong>the</strong> RF here combines <strong>the</strong> uncertainty in<br />

calculating <strong>the</strong> ozone or water vapor perturbation with that from calculating <strong>the</strong> radiative<br />

imbalance.<br />

http://www.ipcc.ch/ipccreports/sres/aviation/068.htm (7 von 8)08.05.2008 02:42:53<br />

Figure 6-6: Fossil fuel use (Gt C yr -1 ) shown for<br />

historical aviation use (1950-92, solid line) <strong>and</strong> for<br />

projected aviation scenarios Fa1 <strong>and</strong> Eab. Total<br />

historical fossil fuel use <strong>and</strong> <strong>the</strong> projection according<br />

to scenario IS92a are also shown.

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