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|    sci.space.policy    |    Discussions about space policy    |    106,651 messages    |
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|    Message 105,628 of 106,651    |
|    Snidely to All    |
|    Re: Starhip goes to 9 engines    |
|    20 Dec 21 15:37:54    |
      From: snidely.too@gmail.com              JF Mezei pounded on thar keyboard to tell us       > On 2021-12-20 16:19, Snidely wrote:       >       >> The extra engines are not the sea level engines, they are the 3       >> additional vacuum engines (RVACs). You don't need sea level engines       >> in LEO, you only need them during launch and landing. But they are       >> still useful in orbit, despite reduced efficiency.       >       >       > Does adding mass for 3 additional engines matter much in the grand       > scheme of things? I recall criticism of Space Shuttle having to       > accelerate its SSMEs to orbital speed as dead weight since it was OMS       > that did the work.       >       > I gather this is some fancy equation of accelerating with lighter mass       > (6 engines) vs accelerating with higher mass ( 9 engines) but greater       > thrust. But those extra 3 engines still have to be lifted from ground       > before they kick in.       >       > Do second stages typically have to throttle back to maintain comfortable       > 3G when there are humans on-board?              Yes.              > Curious to see if the existing 6       > engiunes can reach that 3G easily after being dropped off in semi orbit       > bu the booster, or whether they really need those extra 3 to reach 3G.              It depends on the payload, no doubt. We'll know more about the 3+3       configuration early in the New Year, it seems.              > In terms of lunar lander, I was under the impression that the "main"       > engines would be used for orbital ops, and the "side mounted" thrusters       > would be used in proximity of lunar ground (last stage of landingk first       > stage of taking off).              It appears you acquired an accurate impression. However, that design       may still be in play, or it may have been dropped.              > BTW, if the Raptors can't be used to land on the Moon where regolith       > obeys laws of physics (pushed sideways) could they be used to land on              Pushed sideways is an oversimplification even in vacuum.              > Mars where the atmosphere causes the dust/rocks to behave more       > unpredictably?              The dust and rocks on Mars still obey the laws of physics. Details of       how to land a large rocket on Mars are still under investigation. Some       of the possibilities have already been discussed here, such as adding       aluminum [compounds?] to the exhaust as way to make the landing site       less loose.              /dps              --       Rule #0: Don't be on fire.        In case of fire, exit the building before tweeting about it.       (Sighting reported by Adam F)              --- SoupGate-Win32 v1.05        * Origin: you cannot sedate... all the things you hate (1:229/2)    |
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