Physicist at NTT Research Physics & Informatics Lab. Interested in quantum information, decoherence, rigorously defining wavefunction branches, and classically undetectable soft-particle detection.
Postdocs at IBM Research (under Charlie Bennett) and at Perimeter Institute. UCSB Ph.D. 2012 (advisor: Wojciech Zurek). Princeton B.A. 2007. TJHSST 2003.
jessriedel.com
The premise of this question is wrong, and it's super disappointing that everyone is giving answers as if it's correct. The Honda test rocket only went to an altitude of 300 meters. It's been possible to propulsively land rockets from such low altitudes for decades, e.g., McDonnell Douglas DC-X test in 1996. (And ofc, if you're just talking about re-use for any landing method, the space shuttle first reused the solid rockets and the orbiter in 1981.)
Reusable, propulsively landed stages for rockets capable of putting payloads into Earth orbit is stupendously harder. The speeds involved are like 10-100x higher than these little hops. The first stages of Falcon 9 and Starship are still the only rockets that have achieved that. Electron has only re-used a single engine.
I am deeply looking forward to the dragonfly mission to Titan, since we'll finally get high-resolution color images from the surface, which has liquid seas of hydrocarbons like methane and ethane at -290 F.
https://en.wikipedia.org/wiki/Dragonfly_(Titan_space_probe)
The single image from the surface by the Huygens probe leaves a lot to be desired.
https://en.wikipedia.org/wiki/Titan_(moon)#/media/File:Huyge...
Like the interior of the planet, the atmosphere is overwhelmingly hydrogen and helium. And helium is liquid even at 0 temperature unless under pressure, so presumably (?) would be liquid on the surface. These materials are mechanically very different than the silcates and metals dominating the Earth’s crust, and I don’t think we even have well measured bulk properties? Not sure what erosion processes would look like.
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