|
Read Full Article (file size: 310722 bytes) Cited by
JOURNAL OF GEOPHYSICAL RESEARCH,
VOL. 108, NO. D3,
4103,
doi:10.1029/2002JD002614,
2003
Potential impact of subsonic and supersonic aircraft exhaust on water vapor in the lower stratosphere assessed via a trajectory
model
Gary A. Morris
Department of Physics and Astronomy,
Rice University,
Houston,
Texas,
USA
Joan E. Rosenfield
GEST Center,
University of Maryland Baltimore County,
Baltimore,
Maryland,
USA
Mark R. Schoeberl
Laboratory for Atmospheres,
NASA Goddard Space Flight Center,
Greenbelt,
Maryland,
USA
Charles H. Jackman
Laboratory for Atmospheres,
NASA Goddard Space Flight Center,
Greenbelt,
Maryland,
USA
Abstract
We employ a trajectory model to assess the impact on the stratosphere of water vapor present in the exhaust of subsonic and
a proposed fleet of supersonic aircraft. Air parcels into which water vapor from aircraft exhaust has been injected are run
through a 6-year simulation in the trajectory model using meteorological data from the UKMO analyses with emissions dictated
by the standard 2015 emissions scenario. For the subsonic aircraft, our results suggest maximum enhancements of ∼150 ppbv
just above the Northern Hemisphere tropopause and of much less than 50 ppbv in most other regions. Inserting the perturbed
water vapor profiles into a radiative transfer model, but not considering the impact of additional cirrus formation resulting
from emissions by subsonic aircraft, we find that the impact of subsonic water vapor emissions on the radiative balance is
negligible. For the supersonic case, our results show maximum enhancements of ∼1.5 ppmv in the tropical stratosphere near
20 km. Much of the remaining stratosphere between 12 and 25 km sees enhancements of greater than 0.1 ppmv, although enhancements
above 35 km are generally less than 50 ppbv, in contrast to previous 2-D and 3-D model studies. Radiative calculations based
upon these projected water vapor perturbations indicate they may cause a nonnegligible impact on tropical temperature profiles.
Since our trajectory model includes no chemistry and our radiative calculations use the most extreme water vapor perturbations,
our results should be viewed as upper limits on the potential impacts.
Published 6
February
2003.
Index Terms: 0341 Atmospheric Composition and Structure: Middle atmosphere—constituent transport and chemistry (3334); 1610 Global Change: Atmosphere (0315, 0325); 3334 Meteorology and Atmospheric Dynamics: Middle atmosphere dynamics (0341, 0342); 3337 Meteorology and Atmospheric Dynamics: Numerical modeling and data assimilation.
Read Full Article (file size: 310722 bytes) Cited by
Citation: Morris, G. A., J. E. Rosenfield, M. R. Schoeberl, and C. H. Jackman
(2003),
Potential impact of subsonic and supersonic aircraft exhaust on water vapor in the lower stratosphere assessed via a trajectory
model,
J. Geophys. Res.,
108(D3),
4103,
doi:10.1029/2002JD002614.
Copyright 2003 by the American Geophysical Union.
|