This is interesting in terms of the re-entry flux that can be expected from Starlink, etc. Also, ablative heat shielding on Starship... https://www.pnas.org/doi/full/10.1073/pnas.2313374120
-- *This e-mail may contain confidential material. If you are not an intended recipient, please notify the sender and delete all copies. It may also contain personal views which are not the views of The Economist Group. We may monitor e-mail to and from our network.* * * *Sent by a member of The Economist Group. The Group's parent company is The Economist Newspaper Limited, registered in England with company number 236383 and registered office at The Adelphi, 1-11 John Adam Street, London, WC2N 6HT. For Group company registration details go to http://legal.economistgroup.com <http://legal.economistgroup.com> * -- You received this message because you are subscribed to the Google Groups "geoengineering" group. To unsubscribe from this group and stop receiving emails from it, send an email to [email protected]. To view this discussion on the web visit https://groups.google.com/d/msgid/geoengineering/059edb98-ab7a-4742-834b-f5f1229dc55bn%40googlegroups.com.
