>Would such a project be particularly volume constrained?
It would be mass constrained because of the sheer cost of getting it all into orbit, even with advanced tech such as space elevator. And more volumne = more mass.
There is a saying in aerospace design along the lines of 'weight breeds weight'. Heavier components necessitate stronger, and therefore heavier, supporting structures.
It would be mass constrained because of the sheer cost of getting it all into orbit, even with advanced tech such as space elevator. And more volumne = more mass.
There is a saying in aerospace design along the lines of 'weight breeds weight'. Heavier components necessitate stronger, and therefore heavier, supporting structures.