So, after 3 months of being off work and completely unable to concentrate, my liver tests are back to only mildly alarming and I'm going back to work on Monday. I've been bored out of my skull and have played more RPGs/strategy games in the last three months than I think I have my whole life before that
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Escape velocity from the Sun at 1 AU is calculated by the formula
v_e = sqrt(2GM/r)
Where
G is the Universal Gravity Constant (6.67428 x 10^-11 (m^3/(kg * s^2))
M is the mass of the Sun (2 x 10^30 kg)
r is the distance from the Sun (1 AU or 1.49598 x 10^11 m)
Or, 29789.06669 m/s. Interestingly, this is only very slightly more than the orbital velocity of the Earth itself.
Ah well, that explains why I haven't seen that configuration anywhere else. Thanks for the insight, as always :)
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Obvious in hindsight, I suppose. Ah well, it's always the stupid mistakes that get ya.
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But even if that's a reasonable solution, I don't think any plausible materials technology is up to it. You're back to tractor beam handwaving. Also, the failure of any of those attaching tethers would be pretty catastrophic.
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If I really wanted to prove how impossible the tether system would be, I could calculate the tensile strength needed for each tether. I suspect that with that orbital velocity, the tensile strength would be literally impossible.
At that point, coming up with artificial gravity seems easier :)
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In fact, after my initial post (and your initial comments), I already added a note about this topic to the main post. For reference, here's the note I added:
After some more thought, I suspect this need for constant station-keeping acceleration may end up being the primary flaw for this configuration. Even if we could find a way of propulsion that didn't use up internal mass (or could possibly recapture and re-use it), it seems likely that it would still require energy. The amount of energy needed to keep the cylinder in place around the star may be more than is gathered by the habitat. Since we don't ( ... )
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