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Note: in this question I'm considering cost in both money and fuel terms, and looking for answers that consider both.

So we know that using chemical rockets to reach the moon, or further into space, costs hugely more in fuel, weight, and money terms, than just aiming for low earth orbit.

That raises a question - how do the fuel budgets and economics work out, if we spent fuel and money to create a low earth orbit starting point for further exploration, and bring fuel and rocket components there from earth, as opposed to doing it direct from earths surface?

(Note that if our deeper space exploration started at earth orbit, it wouldn't need to be nearly as massive as we are used to - it wouldn't need the same fuel or rocket systems, nor streamlining, nor protection against atmosphere. It could also return to earth locality for reuse by any gravity-aided route, however slow and leisurely the route, taking months or years to do so if uncrewed, reducing return/deceleration fuel delta-v needs (on crewed ships, life support on average I guess adds less weight than extra fuel to shorten the trip, so a slow return would be viable?). Equally our earth-to-orbit delivery rocket wouldn't need the kinds of crew protection needed for longer travel in deeper space. So the ships involved are very different too, which makes a big difference as well, I suspect.)

By analogy, when we climb an Everest, usually we don't try to do it direct from our hotel in the nearby town. We create a base camp, lug our gear there, and set off on our more challenging and demanding expedition from that base camp, not from our hotel.

  • What are the practical fuel, money/investment, and weight implications, when the two methods are compared for space exploration?

  • If a LEO "base camp" is better, are two (LEO and further out) even better, or do they hit diminishing returns?

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    $\begingroup$ NASA Tipping Point has awarded money to work out some of the basic engineering problems like fuel storage and transfer in space. The questions about the utility of the Lunar Gateway address some of the issues "further out". Orbit Fab is looking to make "gas stations in space", but to extend the lifetime of existing satellites. $\endgroup$ – Schwern Jan 17 at 22:04
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    $\begingroup$ Related, but not a duplicate: Where did Heinlein say “Once you get to Earth orbit, you're halfway to anywhere in the Solar System”? $\endgroup$ – David Hammen Jan 18 at 10:45
  • $\begingroup$ The main barrier for a "orbital space basecamp" is development cost. For spacecraft usually the development is the most expensive part, and most of money are spent even before the launch. So the space traffic at least should be much higher than now to reach economy on scales. Another concern is safety, especially for crewed spacecraft. With such conservative safety measures as the ISS has currently - the station would probably be ineffective as "space basecamp". $\endgroup$ – Heopps Feb 19 at 6:22
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Whatever is used in space has to be sent up from Earth either way. Missions that can do it with a direct launch should. For missions with greater mass requirements than direct launch can do an orbital depot may be an answer but it adds the complexity and costs of making, supplying and using the depot to that of future missions. Sending up eg the full fuel tank modules that can be assembled into a larger orbit launched rocket may not require any permanent installation.

A big pre-investment would be needed for a dedicated space depot/launch station, that will be hard to justify without demonstrating a clear need.

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  • $\begingroup$ That's not really an answer yet, I'm curious if we have hard data or studies showing how the economic and fuel costs compare. Not a general "it would help but is complex and would need justifying". Can you elaborate and answer the question asked? Thanks! $\endgroup$ – Stilez Jan 20 at 5:37

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