10
$\begingroup$

MIT Professor Sadoway believes we can make oxygen anywhere on the moon with Molten Oxide Electrolysis (see here and here).

Let's assume that you need to make enough oxygen to sustain an astronaut for 24 hours. You need to make this amount of oxygen in about 8 hours.

If this can't be done, what is the minimum amount of time it would take to produce that much oxygen and how much equipment would this require?

If you believe there is another method besides Molten Oxide Electrolysis that can accomplish this, you are free to suggest it.

$\endgroup$
  • $\begingroup$ There's no point in specifying the time frame. The issue is how much equipment per astronaut. $\endgroup$ – Loren Pechtel Sep 10 '15 at 0:05
  • $\begingroup$ @LorenPechtel I just want to know for one astronaut in this case, and the time frame would matter since I want the amount of oxygen needed for 24 hours stored in advance. $\endgroup$ – called2voyage Sep 10 '15 at 15:06
  • $\begingroup$ Presumably he has some oxygen available, all that matters is that the production rate is faster than the consumption rate. $\endgroup$ – Loren Pechtel Sep 10 '15 at 15:26
  • 1
    $\begingroup$ So long as the cycle length doesn't exceed his oxygen storage it doesn't matter if it's continuous or batch production. $\endgroup$ – Loren Pechtel Sep 10 '15 at 18:36
  • 1
    $\begingroup$ Those papers are pure gold for me for the fuel production aspect. I've looked for this topic before without coming across Sadoway's work. Thanks for the find :) $\endgroup$ – kim holder Sep 12 '15 at 1:48
6
$\begingroup$

You need to make 550 liters of oxygen in 8 hours. On average in the paper provided they made about 400 milliliters of oxygen per hour (throwing out the high and low outliers). That's 3.2 liters per 8 hours. At that rate you'd need 171 times more equipment than they had for this test to make this work.

They also burned through their electrodes quite often, so you'd need a large supply of these or a way to re-coat them locally.

I'd estimate the equipment weighs between 10 and 25 kg. You've got two crucibles as well as heating elements and insulation. You'd get some economy of scale so you'd need between 855kg and 2,000kg per astronaut, assuming a 100% increase in efficiency.

You could also look at CO2 photodissociation. There's been recent research in using ultraviolet light to fully strip CO2 to C and O2. It could be more efficient and simpler; however it is recycling vs adding new oxygen to the environment so that may not fit your criteria.

$\endgroup$
  • 2
    $\begingroup$ Great start to working out the answer. I'm sure the equipment would probably be configured differently for production of this scale, but just as a reference point how much weight would you figure their original test equipment was? It seems to be relatively small to me. $\endgroup$ – called2voyage Sep 17 '15 at 19:52
  • 2
    $\begingroup$ It's not stated in the paper but I would guess between 10 and 25 kg. You've got two crucibles as well as heating elements and insulation. You'd get some economy of scale so I'd guess you'd need between 855kg and 2,000kg per astronaut. I'm assuming 100% increase in efficiency with scaling. $\endgroup$ – Nathan Sep 17 '15 at 20:11
  • $\begingroup$ Would you mind working this comment into the answer? I think this is basically all I need in an answer. $\endgroup$ – called2voyage Sep 18 '15 at 13:35

Your Answer

By clicking “Post Your Answer”, you agree to our terms of service, privacy policy and cookie policy

Not the answer you're looking for? Browse other questions tagged or ask your own question.