SpaceX CEO Elon Musk says AI compute in space will be the lowest-cost option in 5 years — but Nvidia's Jensen Huang says it's a 'dream'

Images from Muon Space
(Image credit: Muon Space)

In addition to hardware costs, power generation and delivery and cooling requirements will be among the main constraints for massive AI data centers in the coming years. X, xAI, SpaceX, and Tesla CEO Elon Musk argues that over the next four to five years, running large-scale AI systems in orbit could become far more economical than doing the same work on Earth.

That's primarily due to 'free' solar power and relatively easy cooling. Jensen Huang agrees about the challenges ahead of gigawatt or terawatt-class AI data centers, but says that space data centers are a dream for now.

Terawatt-class AI datacenter is impossible on Earth

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Anton Shilov
Contributing Writer

Anton Shilov is a contributing writer at Tom’s Hardware. Over the past couple of decades, he has covered everything from CPUs and GPUs to supercomputers and from modern process technologies and latest fab tools to high-tech industry trends.

  • bit_user
    Sometimes, I really wonder just how much Elon believes some of these things vs. just saying them in an attempt to lure investors to buy stock in his companies.

    The article said:
    On paper, space is a good place for both generating power and cooling down electronics as temperatures can be as low as -270°C in the shadow. But there are many caveats. For example, they can reach +120°C in direct sunlight. However, when it comes to earth orbit, temperature swings are less extreme: –65°C to +125°C on Low Earth Orbit (LEO), –100°C to +120°C on Medium Earth Orbit (MEO), –20°C to +80°C on Geostationary Orbit (GEO), and –10°C to +70°C on High Earth Orbit (HEO).
    This entire digression is somewhat pointless, because he's talking about a polar orbit. That's the easiest way to achieve the continuous sunlight that he mentioned (the other being the far less practical solution of parking at a Sun-Earth Lagrange point).

    BTW, ambient temperatures in orbit are also somewhat meaningless, due to the fact that it's a near vacuum. As Elon said, cooling will have to be radiative.
    Reply
  • vanadiel007
    Just calculate how many solar panels would be required to generate the amounts of power he's talking about, and you will realize it's a non-starter.
    Reply
  • Giroro
    https://media.tenor.com/PZiy4RNZZPwAAAAM/tim-curry-space.gif
    Reply
  • Klathra
    If the AI compute satellite needed to radiate 1 terrawatt of energy and you could run it at 127 C it would need to have 690 km² of surface area, assuming a perfectly black surface for emissivity. As temperature goes up the surface area needed goes down, but even if you could somehow get the electronics to survive much higher temperatures the surface area is still far too large.
    Am I missing something?
    Reply
  • SkyBill40
    The efficiency of solar panels would need to make a quantum leap in order to pull off something on this level. That doesn't take into account the other heavy lifting of just getting that mass up there in the first place.

    And then what? How long before it falls behind newly developed architectures? It's not like it's easy to just send people up there on a mission to hardware swap, especially at some of the orbital levels discussed. I mean... just look at how much work it took to get the HST right. That required multiple shuttle missions to correct.
    Reply
  • bit_user
    vanadiel007 said:
    Just calculate how many solar panels would be required to generate the amounts of power he's talking about, and you will realize it's a non-starter.
    I assume the solar panels he'd use would be more efficient, but if we take the example of the ISS, it gets about 100 W/m^2 (source: https://en.wikipedia.org/wiki/Solar_panels_on_spacecraft#Spacecraft_that_have_used_solar_power ). So, 1 TW would require 1 * 10^10 m^2 or about 10,000 km^2 (i.e. 100x100 km array).

    I wonder how much energy it would take to shoot that mass into orbit, and what the break-even point would be for offsetting that initial energy expenditure vs. just using ground-based solar.
    Reply
  • vanadiel007
    bit_user said:
    I assume the solar panels he'd use would be more efficient, but if we take the example of the ISS, it gets about 100 W/m^2 (source: https://en.wikipedia.org/wiki/Solar_panels_on_spacecraft#Spacecraft_that_have_used_solar_power ). So, 1 TW would require 1 * 10^10 m^2 or about 10,000 km^2 (i.e. 100x100 km array).

    I wonder how much energy it would take to shoot that mass into orbit, and what the break-even point would be for offsetting that initial energy expenditure vs. just using ground-based solar.

    Exactly, which does not even take into account the herculean task of assembling that in space, and ensuring space debris does not destroy it once it's fully "deployed".

    And while I am far from a space expert, I am thinking such a structure would cast a huge shadow over earth and likely be visible with the naked eye.

    It would likely be much more practical and less costly to generate that power here on good old earth.
    Reply
  • bit_user
    SkyBill40 said:
    The efficiency of solar panels would need to make a quantum leap in order to pull off something on this level.
    Spacecraft typically use more exotic panel technology than terrestrial applications, I think because it's a lot more economical to launch a smaller panel for a given output level, even if it costs more to manufacture.
    https://en.wikipedia.org/wiki/Solar_panels_on_spacecraft#Types_of_solar_cells_typically_used
    SkyBill40 said:
    And then what? How long before it falls behind newly developed architectures? It's not like it's easy to just send people up there on a mission to hardware swap, especially at some of the orbital levels discussed.
    Oh, that's where his Optimus robots enter the picture!
    🤖
    SkyBill40 said:
    I mean... just look at how much work it took to get the HST right. That required multiple shuttle missions to correct.
    That was also 40 years ago. Most satellites don't need field maintenance. Due to its orbit, it would be virtually impossible to send a manned service mission to JWST, which is far more complex than Hubble.


    (if this image doesn't load, see it here: https://www.space.com/james-webb-space-telescope-secondary-mirror-deployed )
    Reply
  • bit_user
    vanadiel007 said:
    And while I am far from a space expert, I am thinking such a structure would cast a huge shadow over earth and likely be visible with the naked eye.
    It wouldn't cast a shadow if it's in a polar orbit that aligns with the dusk/dawn boundary. That's what it would have to use for 24/7 sunlight. Otherwise, you'd need to add batteries, which would be a whole lot more mass to launch and something else that needs maintenance/replacement.
    Reply
  • hotaru251
    so more space litter?
    Reply