starcraftre

starcraftre t1_jdx6l14 wrote

Assuming a 1 AU sphere for the original design spec, and assuming you want statites, then your target areal mass is around 1.6 g/m^2 .

Taking my 10% coverage estimate, the factored surface area of a 1 AU sphere is 2.81e22 m^2 or 4.5e19 kg of material. 2% of the Belt, assuming every rock is made of aluminum.

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starcraftre t1_jdw12xv wrote

So, the article takes the pop culture version of a Dyson Sphere (big solid ball kilometers thick), rather than the actual original definition (lots of really low-mass satellites/statites), and concludes it isn't viable.

Meanwhile, the original definition only "loses" 1 order of magnitude of energy collected (~10% coverage), while requiring 16 orders of magnitude less energy to build and place.

Not to mention the maintenance costs of a kilometer-thick shell is astronomical compared to a bunch of millimeter-thick mirror sails (which you can just replace for pennies).

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starcraftre t1_iuvu6qh wrote

That really doesn't support the claim that they're much farther ahead. TU did physical demonstrations of how they'll print structures using their Trusselator about 8 years ago, and have had their printing/recycling prototypes on the ISS for 4 years (launched on the S.S. John Young Cygnus flight). Actual microgravity testing, not just simulated.

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