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|    sci.space.policy    |    Discussions about space policy    |    106,651 messages    |
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|    Message 105,118 of 106,651    |
|    Snidely to All    |
|    Re: Test flight altuitude    |
|    23 Jan 21 21:10:10    |
      From: snidely.too@gmail.com              JF Mezei explained on 1/23/2021 :              > SN8 was tested to 12.5km and highly succesfull from launch right up       > until landing legs touch ground.       >       > I am curious on why SN9's test flight would be an indetical repeat       > instead of pushing the limits in the areas whene SN8 aced its test.              I've actually heard that a lower (10km) apogee will be used, and the       speculation is that it is to improve the chances of favorable winds       aloft [during this winter season].              From the Boca Chica dailies, it is clear that the beach gets additional       less-than-holiday weather at this time of year.              > Would it be correct to state that whether you drop from 12 or say 50km,       > you reach terminal velocity and you have the same vertical speed at the       > time you do the final manouver to turn ship and land?       >       > If SN8 aced the climb to 12.5, why now push SN9 to say 50km?              Because you've only tested the response under one set of weather       conditions?              > Say SN8 started with a tank that was 1/4 full and climbing to 50 would       > require a tank that is half full. Would the longer burn duration and       > the portion of time where the tank is more than 1/4 full intreoduce       > significantly different conditions in terms of pressurizing the tanks       > and feeding fuel/O2 into the engines ?       >       > I am just trying to understand why SpaceX would be so hesitant in       > raising test flight altitude.       >       > I know they really want a succesfull landing ASAP because NASA is       > evaluating moon landing hardsware contracts in Febvriary. And getting       > SN9 do a succesful landing would give SpaceX a pretty big "we already       > have hardware that can land" stamp of approval. But if testing to       > higher altitude changes nothing to the landing, why not make this       > "iterative design" coincide with iterative testing?              Falcon 9's landing track record counts for nothing? And SN8 was       clearly capable of sticking the landing with just a little more header       pressure. I don't think that will be ignored in February.              /dps              --       "First thing in the morning, before I have coffee, I read the obits, If       I'm not in it, I'll have breakfast." -- Carl Reiner, to CBS News in       2015.              --- SoupGate-Win32 v1.05        * Origin: you cannot sedate... all the things you hate (1:229/2)    |
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