As
the U-2 with a payload of ~2.5 tons is the only viable delivery method
for current SAG modelling at these altitudes, deploying 20 Mt of SO2
precursor annually, for example, would require ~ 8 million flights per
year, or ~22,000 flights per day.
The
winds at these levels are light and variable, reverse direction
unpredictably and would not distribute aerosol evenly (see examples of
winds today 1/09/2024 and one year ago at 70mB and 10mB https://earth.nullschool.net
If you access the site the aninimation will show the changes in wind
strength and direction more clearly ) . The idea that the aerosol would
be uplifted by the Brewer-Dobson circulation or spread evenly zonally
from one or several injection points is not borne out by our current
limited knowledge of circulation in the stratosphere.
It
would be impossible to monitor which levels of the stratosphere had
sufficient concentration and which parts needed more aerosol added. some
regions would get a excess aerosol and some areas would be missed due
to the variability of the upper level winds.
All
aircraft flying in the lower stratosphere, i.e. commercial, military
and geoengineering aircraft, would be in a flying through a sulphuric
acid atmosphere and this would incur damage to the planes and engines.
There
would be always be a large concentration gradient between the injection
points and the areas distant from that point giving uneven cooling. The
cooling effect will be less than theoretically modelled due to rapid
coagulation and sedimentation in the areas with too much aerosol, and
also less than theoretically modelled in the areas with have less than
optimum aerosol concentrations.
Injection
of SO2 would use up hydroxyl radicals which would otherwise oxidise
methane (see Tilmes et al 2018) It is worrying that although Tilmes et
al recognised this in 2018, none of the Stratospheric Aerosol
Geoengineering) (SAG) papers since then have discussed this issue.
Regards, Colin