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Title: Subsidence of aircraft engine exhaust in the stratosphere: Implications for calculated ozone depletions

Journal Article · · Geophysical Research Letters (American Geophysical Union); (United States)
DOI:https://doi.org/10.1029/93GL03426· OSTI ID:5050005
; ; ; ;  [1]; ;  [2]
  1. Atmospheric Environmental Research, Inc., Cambridge, MA (United States)
  2. Aerodyne Research, Inc., Billerica, MA (United States)

The deposition altitude of nitrogen oxides and other exhaust species emitted by stratospheric aircraft is a crucial parameter in determining the impact of these emissions on stratospheric ozone. The authors have utilized a model for the wake of a High-Speed Civil Transport (HSCT) to estimate the enhancements in water and reductions in ozone in these wakes as a function of time. Radiative calculations indicate differential cooling rates as large as -5K/day at the beginning of the far-wake regime, mostly due to the enhanced water abundance. These cooling rates would imply a net sinking of the wakes of about 1.2 km after three days in the limit of no mixing. Calculated mid-latitude column ozone reductions due to emissions from a Mach 2.4 HSCT would then change from about-1% to -0.6%. However, more realistic calculations adopting moderate mixing for the wake reduce the net sinking to less than 0.2 km, making the impact of radiative subsidence negligible. 15 refs., 3 figs., 1 tab.

OSTI ID:
5050005
Journal Information:
Geophysical Research Letters (American Geophysical Union); (United States), Vol. 21:1; ISSN 0094-8276
Country of Publication:
United States
Language:
English