Getting back to this again…
I rechecked the math in that post, and everything was fine until the very last line! The E/d[sup]2[/sup] of diamond is not 0.1; it’s nearly 100,000. That’s still a far cry from the necessary 450k+, but we can work with that.
Instead of solid diamond, we’ll use an octet space frame of diamond rod. Since macroscopic buckling is the main constraint, I’ll work from there and then double-check at the end that the other constraints are met.
The space frame in question is composed of octahedrons, and a unit cell consists of length 12 of rod material, with a volume of 1.414, a cell mass of 12pir[sup]2[/sup], and a density of 26.66r[sup]2[/sup]. We’ll also keep in mind a “derating factor” of 8.89r[sup]2[/sup], which is the factor we divide the force on the unit cell by to get the force on the component members (this is just the cross-section of each rod, times 4, divided by sqrt(2)). Or, we might multiply by that number to get the effective limits on a unit cell.
We’ll start with the high-end estimate from before, to allow some margin (especially given that the space frame is not perfectly isotropic; it’s pretty close but not 100% along all axes):
E/d[sup]2[/sup] = 1500000
Our members are made from diamond, which has E=1.22e12 Pa and d=3520 kg/m[sup]3[/sup]. Therefore, for the space frame:
E = 1.22e128.89r[sup]2[/sup] = 1.085e13r[sup]2[/sup]
d = 26.66r[sup]2[/sup] * 3520 = 93800*r[sup]2[/sup]
So:
E/d[sup]2[/sup] = (1.085e13r[sup]2[/sup])/(93800r[sup]2[/sup])[sup]2[/sup] = 1500000
(1.085e13r[sup]2[/sup])/(93800r[sup]2[/sup])[sup]2[/sup] = 1500000
8.22e-4 = r[sup]2[/sup]
r = 0.0287
Ok, not too bad. That r is unitless, by the way–we’re considering it as a ratio. But it means if we built the truss out of 1 m rods, they would have to be 5.7 cm in diameter to meet our requirements. That’s pretty slender, as we’d expect, but not absurdly so.
This material won’t buckle “macroscopically”, but what about the individual components? Specifically, will the rods themselves buckle or otherwise fail?
To make things easier, lets assume a 1x1x1.414 m unit cell (again, all of this is scale-free, so it doesn’t matter if we scale down to micrometers at the end).
The thickness ratio from zut was just:
(t/R) = 0.43/d
We know d; it’s 26.66*r[sup]2[/sup]*3520, so d=77.3, and (t/R)=0.0056.
Hoop stress is:
S = qR/2t = (q/2)/(t/R) = (101325/2)/0.0056 = 9050000 Pa.
We’re considering a 1m cell, so the force is 9050000 N, and the effective force on each member is 3200000 N.
Let’s look at the buckling limit of each member. Euler’s critical load formula for columns is:
F = pi[sup]2[/sup]EI / (KL)[sup]2[/sup]
I is the moment of inertia; we have a circular cross-section, so it’s (pi/2)r[sup]4[/sup]. K is 0.5 since the column is supported on both ends. E is that of normal diamond. L is 1. Therefore:
F = pi[sup]2[/sup]1.22e125.33e-7 / 0.25 = 51330000 N.
That’s 51 MN, and we only needed 3.2 MN. So that’s plenty. What about basic compressive strength? Diamond has a compressive strength of 110 GPa, which comes to 284 MN for our rod. Way more than plenty.
So I’m going to call this plausible. The raw compressive strength is so high that there’s plenty of margin in that regard. We could have reduced the structural member diameter by a fairly large factor and still have compressive margin left over; the lowered density would increase the E/d[sup]2[/sup] even further, but that doesn’t appear to be necessary. I did make some assumptions with regard to the isotropy of the space frame but nothing that would make even a 2x difference, and there is enough margin everywhere to account for that.
All that we need now is a few hundred cubic meters of perfect diamond and a system to machine it down with micrometer precision. Easy.