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|    sci.space.policy    |    Discussions about space policy    |    106,651 messages    |
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|    Message 105,125 of 106,651    |
|    David Spain to JF Mezei    |
|    Re: Test flight altuitude    |
|    25 Jan 21 09:43:25    |
      From: nospam@127.0.0.1              On 1/24/2021 4:40 PM, JF Mezei wrote:       > On 2021-01-24 08:03, Jeff Findley wrote:       >       >> Because standard experimental practice is to only change one variable so       >> you can compare the results of two tests. In this case, they've made       >> changes which impact the final landing burn.       >       >       > Hence my question on whether terminal velocity at time of final landing       > sequence would be the same whether you launch to 50 or 10. If it is the       > same, wouldn't it be fair to state that a test to 50km would have       > identical conditions at the time of the final landing sequence?              I don't think so. To get to 50km you need more propellant than to 10km.       If you are studying/testing internal tank pressure (head pressure) you       might want to profile at different propellant loads. Since the last test       at given propellant load X failed, you'd probably want to re-test with       the same load factor. If successful then move on to Y. Note that if       successful, and the engines/tanks etc. aren't damaged in any significant       way, the next flight can take place quickly. Here quickly means weeks       not months.              >       > With regards to winds, does this mean a "cold turkey" escalation from       > 10km up/down to orbital because higher than 10/12 km, you get winds       > that exceed cross range capability?       >              Doubtful. Propellant load should be able to handle whatever altitude you       are testing for. Winds aloft will be known ahead of time, so that should       provide limit bars for cross range. BTW, Elon has tweeted in the past       the cross range of a typical sub-orbital Starship is on the order of       10,000 km, that's for coming down from well above these test altitudes       however. The cross range for these tests is, comparatively speaking,       quite limited I'm sure. But that's fine, even if lost, these are test       vehicles, easily replaced.              > For testing of starship, would an alternate landing side be in the plans       > to allow mid altitude testing with landing elsewhere ?              Doubtful, until he gets those oil rig platforms converted and presumably       placed at various spots in the Gulf of Mexico. There aren't any Starship       landing sites yet at the Cape (or anywhere else) for the time being.       Maybe in a year or two?              Dave              --- SoupGate-Win32 v1.05        * Origin: you cannot sedate... all the things you hate (1:229/2)    |
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