Classification: Unclassified >I meant that JPL was worried about that for Mars landers. And it may >not be "we know it will be a problem." It may be more like "We can't >prove it won't be a problem."< Indeed, that was my point. A nice paper summarising the knowledge gap and approaches to filling it: <http://www.ssdl.gatech.edu/papers/conferencePapers/AIAA-2010-5046.pdf> It includes suborbital rocket tests and balloon-launched test as possible solutions. These slides suggest 60km (~180kft) so maybe a bit sporty for an amateur rocket: <https://solarsystem.nasa.gov/docs/02_Supersonic%20Retropropulsion%20Technology%20Development%20in%20NASA's%20Entry,%20Descent,%20and%20Landing%20Project_K.%20Edquist1.pdf> This paper has more detail on potential use of Terrier variants (at 40-50 km altitude): <http://www.planetaryprobe.org/sessionfiles/session4/papers/post_srp_ft_concepts-paper.pdf> More relevant stuff here: <http://www.google.co.uk/search?hl=en-GB&source=hp&q=supersonic+retropropulsion> Alex Aplin "Personal e-mail. This e-mail is personal. It is not authorised or sent on behalf of Dstl. This e-mail is the personal responsibility of the sender." "The remarks in this e-mail are personal and do not represent Dstl or Government policy." "This e-mail and any attachment(s) is intended for the recipient only. Its unauthorised use, disclosure, storage or copying is not permitted. Communications with Dstl are monitored and/or recorded for system efficiency and other lawful purposes, including business intelligence, business metrics and training. Any views or opinions expressed in this e-mail do not necessarily reflect Dstl policy." "If you are not the intended recipient, please remove it from your system and notify the author of the email and centralenq@xxxxxxxxxxx"