MUSKSAYS

Latest posts · Page 2372

  1. 8,180 likes

    @officialsusq Exactly

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  2. 16,257 likes

    @Zanfa I do like nonsense memes. It’s true.

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  3. 263,541 likes

    Yes https://t.co/3KoZ13fQEz

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  4. 15,019 likes

    @Lebeaucarnews https://t.co/W60sKBdLPz

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  5. 17,929 likes

    @lexiheft @MrBeastYT Next few days

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  6. 59,758 likes

    💩 looks like sentient choc ice cream

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  7. 110,136 likes

    Just bought https://t.co/LJJCD7BAgX oh yeah

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  8. 1,810 likes

    @ukrpravda_news Whoa cool

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  9. 4,694 likes

    @vincent13031925 @Tesla No plans to do so. Would recommend Model S.

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  10. 988 likes

    @Trump_45th @SpaceX 7

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  11. 6,558 likes

    @royalsociety @GreshamCollege ♥️ logarithms

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  12. 2,125 likes

    @Archin50001 @AlexTheChemist @SpaceX Dammit! 😀

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  13. 620 likes

    @122ddd2223d @Dash71209069 @yungmruglygod @nickynaptime We’ll tweak the alloy over time, so it won’t exactly be 301, but close

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  14. 3,056 likes

    @AlexTheChemist @SpaceX Well, my past mistakes do seem extremely dumb, especially the ones where I mistakenly thought I was smart

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  15. 656 likes

    @nickynaptime Rocket mass ratio is about the same for aluminum-lithium vs 301 stainless full hard at cryo, but latter costs way less, is tougher & doesn’t even need paint!

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  16. 970 likes

    @SpaceXFan97 @wonderofscience @Treebeard1671 @Erdayastronaut @keego73 Still up to 31. Will probably fly with fewer initially in case it blows up.

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  17. 675 likes

    @wonderofscience @Treebeard1671 @Erdayastronaut @keego73 Mostly true

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  18. 1,110 likes

    @Erdayastronaut @keego73 Cold gas thrusters only. Will use body flaps & main engines for landing orientation, so won’t need high thrust reaction control. Simplifies things considerably.

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  19. 1,010 likes

    @TriTexan @SpaceX Yes

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  20. 19,696 likes

    Initially making one 200 metric ton thrust engine common across ship & booster to reach the moon as fast as possible. Next versions will split to vacuum-optimized (380+ sec Isp) & sea-level thrust optimized (~250 ton).

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