Elon Musk

@elonmusk ↗

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Last Checked April 2, 2021

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Wed Jun 10 17:58:30 +0000 2020

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Elon Musk @elonmusk

@SciGuySpace Combined with SpaceX deep subcooling of propellants to near liquefaction temp of N2, use of common dome (CH4 & O2 liquid at similar temps) & higher T/W of engines enables de facto higher delta-V than an H2/O2 stage — PolitiTweet.org

Posted June 10, 2020 Hibernated

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Elon Musk @elonmusk

@SciGuySpace Quite a piece! I should credit Soviet/Russian engine work in the 80’s as being a factor in deciding to switch from H2 to CH4. They demonstrated excellent performance on test stands, with Isp up to 380 secs. — PolitiTweet.org

Posted June 10, 2020 Hibernated

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Elon Musk @elonmusk

@venus47203379 @engineers_feed Haha. Will post summary. — PolitiTweet.org

Posted June 10, 2020 Hibernated