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zolotiyeruki

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Posts posted by zolotiyeruki

  1. I'm not terribly concerned about the "landing between towers" issue, because:
    1) The towers are likely to be removed.  They were originally designed for drilling oil wells, and are unlikely to be suitable for SpaceX's operations.  In fact, very little of the existing topsides equipment and structure are likely to be useful.  These rigs are going to get stripped down.
    2) F9 landings are remarkably accurate, and I believe the same will become true for SS.  Heck, with their two attempts to date, they've already been really close.
    3) Any new towers could retract a la F9's strongback
    4) OCISLY endured multiple hard landings.  Sure, SS/SH will be dramatically heavier, but the fact remains that you can build a structure to take it.

  2. 28 minutes ago, Jacke said:

    I find Starship fascinating.  As a cargo vessel, because with all launch vehicles still having a minimum failure rate of 1-2%, having no launch escape system and crewing it would means condemning some future crews to die.  I also think using it to go to the Moon is marginal and to Mars is even less so, being it is designed and optimized to get to LEO.

     

    Sure, if you were designing a rocket specifically to go to the moon, you could make it significantly more efficient than Starship.  But fuel is relatively cheap, and even though the cargo part of the spacecraft would need engineering, you'd be starting with a propulsion and landing section (engines, tanks, control systems, etc) that is already proven.

  3. "Master the flip"?  It seems to me that they've already got a pretty good handle on the maneuvering algorithms.  They're 2 for 2 on that part.  It's the engines that are currently giving them trouble.

    Speaking of which, did SpaceX ever say why the second engine didn't light on SN9?

  4. 4 hours ago, wumpus said:

    Presumably Spacex intends to obsolete Falcon Heavy with Starship as fast as they can, but it is nice to see that a launch vehicle that is already in production and relatively inexpensive get more capability.

    For stuff going beyond LEO, wouldn't SS's payload have to include whatever stage is necessary to take the real payload to its final destination?  Or are SpaceX planning to build SS so that it can re-enter from GTO?

  5. 1 hour ago, sevenperforce said:

    The tiles have gaps between them, so it's fairly straightforward to wrap the tile matrix around a cone as long as you mind the gap.

    Untitled.png

    As you can see, the angle starts four tiles down but the gaps are large enough that the bent-over tile sections (unbent tiles on right) don't collide. Wherever there is a collision you take out that tile and you use a large, single, customized tile to fill that particular space. 

    If you don't want to use a customized piece then you can just tile the space irregularly and allow larger gaps. 

     

    Another option is to switch to slightly-trapezoidal tiles for the nose section, and arrange them in rows.  That way, you only have three types of tiles: hexagonal for the cylindrical portion, half-of-a-hexagons at the joint between the rings and the nose cone, and trapezoid.

  6. 5 minutes ago, Elthy said:

    SpaceX still has a problem, even if they try the three engine burn next time. If the issue was with the fuel supply another engine wouldnt help, if the problem was in the engine itself then they seem to have issues with Raptors reliability. The second one is propably worse, since those are way more complex to develop/modify.

    It quickly becomes a question of whether it makes more sense to improve the design to prevent failures due to external factors, or increase the redundancy to mitigate the failures.  In the case of Sn8, you definitely want to improve the fuel system so as to not starve your engines.  If a very speedy bird flies up the engine bell, that might be something you address by lighting three engines instead of two.

  7. Two thoughts about the recent starlink mission:

    1) As I recall, the F9 reuse goal was 10 flights.  They now have a booster that has hit 8.  Dang, that's impressive, and dang, that's a lot of money saved.
    2) In some of the early landing attempts, SpaceX tried some 1-3-1 landing burns, and there was speculation of a 3-engine hoverslam, as an optimization to squeeze a bit more payload into orbit.  Why did they abandon those efforts?

  8. I started poking around, and was able to get a "zero" button in place and working, but the layout is messed up.  I don't know if I'll be able to get it working in EVA construction mode.  As I said before, I'm a complete noob at mods, although I have lots of experience programming.  It only took me about half an hour to sort out the code and figure out how to add the zero button.

  9. I'm not terribly concerned about landing accuracy--the last few dozen F9 boosters look to have landed within a meter or so of dead center on the landing pad.  There aren't many last-second failure modes, and SpaceX have found many already (running out of hydraulic fluid for the gimbals, low header tank pressure, out of fuel during the hoverslam, etc), and there's not much fuel left to go boom at that point anyway.  Not that I wish to minimize the damage that 200 tons of stainless steel can do when falling at dozens of meters per second, but we're not talking about a massive explosion even if something *does* go wrong.

    The ability to hover makes this considerably easier as well, because it means that cm accuracy isn't necessarily required during the landing burn--it can hover and translate as needed for a few seconds.

    It still sounds bonkers, though.

  10. 1 hour ago, Nightside said:

    Yep. But do we expect the CoM to really be that high? What is the expected dry mass and payload these days?

    Keep in mind, though, that regardless of the use case on earth, the eventual goal is to land these on Mars, then refuel and return.  Depending on the mass of the payload up front, filling the fuel tanks may shift the CoM towards the nose (or toward the rear!).

    Speaking of which, was there a mass simulator in the nose of SN-8, or was it just a hollow shell?

    31 minutes ago, cubinator said:

    We all know what happens when you fly a fuel tank that was dropped...

    As I recall, it wasn't a dropped tank, it was a change in the voltage spec for some instrument or tank heater.

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