http://www.nzz.ch/wissen/wissenschaft/sonnenschutz-fuer-die-erde-1.17282213
_______________
Ken Caldeira
Carnegie Institution for Science
Emeritus Professor of Engineering Design Institute for Energy Systems School of Engineering Mayfield Road University of Edinburgh EH9 3JL Scotland Tel +44 131 650 5704 Mobile 07795 203 195 www.see.ed.ac.uk/~shs
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30 hPa is about 25kms. That's pretty normal for release studies. See for example Aurora flight services report
I'm doing a paper at present which shows you can loft a shell that high for very little money - probably an order of magnitude cheaper than Aurora calculated. I've not finished the calcs yet.
You could hit those costs using an extended Mark 7 Iowa class 16 in gun. Methane/air propellant should get you to 25k, but using a H2 / O2 propellant (run rich) can get far higher by improving speed of sound. To cut shell mass you can use an enlarged, fin-stabilized aluminum or titanium shell. Projectiles would splashdown, to be reused or scrapped.
A
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<mailto:kcaldeira@__carnegiescience.edu
<mailto:kcaldeira@carnegiescience.edu>>
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*Currently visiting * Institute for Advanced Sustainability
Studies
(IASS) <http://www.iass-potsdam.de/>
*and *Potsdam Institute for Climate Impact Research (PIK)
<http://www.pik-potsdam.de/>*__in Potsdam, Germany.*
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