http://www.grida.no/climate/ipcc_tar/wg3/176.htm

"In principle, only ~10^5t of such mesh structures are required to
achieve the benchmark 1% increase in albedo."

http://www.ucalgary.ca/~keith/papers/26.Keith.2000.GeoengineeringHist...

"Teller et al (8) note that a scattering system at the L1 point need
only deflect light through the small angle required for it to miss the
earth, about 0.01 rad as compared to  1 rad for scatterers in near
earth orbit or in the stratosphere..."

You missed Keith's preceeding comment about positioning such a "system"
at L1.  He noted that:

   " The obvious geometry is a fleet of shields in low-earth orbit
(NAS92). However, solar shields act as solar sails and would be pushed
out of orbit by the sunlight they were designed to block. The problem
gets worse as the mass density is decreased in order to reduce launch
costs. A series of studies published in 1989–1992 proposed locating
the shield(s) just sunward of the L1 Lagrange point between the Earth
and sun, where they would be stable with weak active control."

That phrase "active control" is the problem.  Control implies structure
to keep the mass together while force(s) are applied to counter the
effects of solar wind and solar pressure.  Those forces must be
produced by reaction, ie, rockets that throw away mass.  Even electric
propusion requires some source for the mass being thrown overboard and
some additional mass to produce the electricity, perhaps PV cells.
Supplying all this mass would require servicing and constant
maintenance for as much as 1,000 years after the fossil fuels are gone.


Building something this large would make the Space Station look like a
flea.  Providing this is very expensive with today's technology.  Your
off-hand comment about costs is silly, as this alternative looks
grossly expensive to me.


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