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Cake day: February 28th, 2024

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  • My uneducated guesses:

    1. Starlink’s existing provision for Earth could be achieved for Mars too, using a very similar system
    2. In some ways, Mars will be easier.
      1. Much thinner atmosphere
      2. Far fewer of the constraints needed to ‘play nice’ with an existing high-tech civilization, like minimizing reflections of sunlight to the ground, or avoiding radio interference.
    3. But the first generation system for Mars will be different in an important way: significantly higher altitude
      1. Thus higher ping times
      2. And fewer satellites than would otherwise be needed for continuous coverage, which in turn means lower total bandwidth capability, and less redundancy, but much cheaper & quicker to set up and maintain.
    4. None of the above covers the actual NASA requirement/aspiration for new interplanetary comms (which seems to be referred to as “DRM 4”).
      1. For one thing, an in-space laser link that can cover 100s of miles efficiently, is qualitatively different from one that can cover 100s of millions of miles.
      2. But as NASA has already achieved over 6 Mbps across 240 million miles, SpaceX will also be able to create a usable interplanetary link
    5. SpaceX will equip some of their Earth-orbiting Starlink satellites, and all of their Marslink satellites, with this qualitatively different, and outward-facing, laser comms tech.
      1. Having, as your endpoints, devices that are orbiting around planets, is disadvantageous in some ways, such as the fact they spend about half the time on the wrong side.
      2. But SpaceX will find a way to make it into an advantage. (Multiple simultaneous connections?)

    Any thoughts?

    Also, you need a relay capability when the sun is in the way. But are such relays expected to be beneficial even at other times? Will SpaceX find a way to make them beneficial?

    P.S. It’s interesting that Spaceflight Now did a tweet thread on this NASA presentation, but didn’t consider it worth an article. Yet PC Mag made a whole article primarily out of 1/3 of a slide from one of those tweets by Spaceflight Now! (And I’m glad they did!)












  • Watched some of the official coverage: https://www.youtube.com/live/5CRB3FHV9Dw

    Things that were new to me:

    • 1:40:50 Drone footage of the capsule lift
    • 34:42 Jones explains that the same set of 12 hooks secures Dragon to either its nosecone or to the ISS. Makes perfect sense; I’d just never thought about it before.
    • 1:35:57 “There are multiple options so if Dragon were to splash down in a different orientation they could egress from the top hatch as well.”
      • Would this be a last resort after they’d tried & failed to correct the orientation?
      • Would it only be used when Dragon was still in the sea or would they ever lift Dragon onto the boat in an orientation that necessitated top hatch egress?

    And all this talk of Dragon orientation, combined with the extensive weather delays in Crew-8’s departure, got me wondering … How would Dragon fare if it was left in very rough seas for an extended period? (Imagine the recovery vessel broke down a minute after splash-down and then a big multi-day storm blew in, or something.)


  • Plausible. It’s not how I imagine them engaging with their defence contractors but I don’t actually have a clue how it works. One supporting point might be if there were any other companies treated similarly, like if Lockheed Martin was ordered to immediately ramp up production of relevant types of military hardware, and told that the details (contracts / payment / etc.) would be sorted out later.

    An opposing point would be the fact that the US and its allies knew an invasion was likely well in advance. Yet the initial Starlink ‘roll out’ seemed pretty ad hoc, with SpaceX organizing its own logistics. But then maybe the allies didn’t expect Russia to be so effective in disrupting the existing military comms infrastructure.