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What is the terminal velocity of starship on earth and mars during descent?

Has SpaceX revealed or hinted the values of projected surface area and drag coefficient of the vehicle?

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  • $\begingroup$ That'll depend on the ballistic coefficient, wchich will depend on the design, control surface position and mass. $\endgroup$ – user20636 Dec 10 '20 at 23:43
  • $\begingroup$ @JCRM And altitude. $\endgroup$ – Russell Borogove Dec 10 '20 at 23:49
  • $\begingroup$ and weather @RussellBorogove $\endgroup$ – user20636 Dec 10 '20 at 23:52
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    $\begingroup$ I'll bet $1.602 \times 10^{-19}$ bitcoin that it's 85$\pm$10% of the terminal velocity of an equivalent right elliptical cylinder of my choosing after the correct answer is posted. $\endgroup$ – uhoh Dec 11 '20 at 0:11
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    $\begingroup$ @uhoh I thought about doing the math, but I'd have to guesstimate mass and look up published dimensions and bleaaaahhhhhhh $\endgroup$ – Russell Borogove Dec 11 '20 at 2:06
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I have been looking for the same thing. The only mention I found was on a blog post (https://www.neowin.net/forum/topic/1402753-spacex-starship-sn8-15km-test-flight/) which stated 66-68 m/s for SN8. If true, that would imply ± 320 m/s on Mars.

Despite Mars' lower value for g (3.72), the much lower atmospheric density of 0.02 versus 1.2 kg/m3 results in a much higher Vt. This of course assumes that everything else remains constant (mass, area, Cd).

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