Might be a dumb question, but...
I recall one of the interesting tidbits about the SR71 construction (also titanium) was that it was specifically engineered in a way that leaked fuel on the ground, necessitating refueling immediately after takeoff, because the speeds / pressures / temperatures at cruising conditions would swell the metal to fill the gaps.
In theory...couldn't you do something in the reverse for a submarine? Ie, engineer it in a way that as the pressure builds, it actually gets stronger / more secure?
I feel like the sphere obviously works, but in this day and age of AI assisted tools, we may see some crazy bulbous / tetrahedron / whatever designs start getting tested with that principle in mind.
that's a heat effect, not really applicable here though there would be some contraction of the materials as they get colder this is a finite amount. for it to be of any use the internal pressure would have to be equal to the external pressure to induce tension in the CF laminate
if one could find a method to do the opposite of pre-stressing concrete, that would be interesting. only thing i could come up with is pressurizing the inside, which is of course impossible because of the meat based passengers
The second vid in ctwo's post claims that the carbon fiber compressed a half inch more than the titanium at operational depths. I have no idea it that is true.
And because I'm that guy:
The SR-71 did leak, and it did require refueling immediately after takeoff. The SR-71 did not takeoff fully fueled because it would not be able to successfully abort the takeoff if there was an emergency due to the added weight of full tanks.
the differential movement is a fact. i didn't check his numbers but they sound likely.
i haven't seen all the videos out there of course, people love to get really verbose about this incident and i'm about to do the same thing. the different rates with with which the rings and tube contract is partcularly bad right next to the joint where there is a slight overlap of the Ti onto the CF, if it were a weld it'd be the heat affected zone where you expect welds to break (just for visualization purposes i use that example, it's otherwise irrelevant)
with the Ti ring effectively not moving, and the center of the CF tube contracting significantly the loading on the glue joint puts a moment load into the skin of the CF tube, which tries to peel the tube apart separating the individual plies from the one next to it. Interlaminar Shear Strength is the name of the property, and it's generally orders of magnitude lower than in the preferential direction. I think that's the initial failure point and it wouldn't have been a pin hole, at least not for any measurable period of time
a similar situation contributed to the Challenger exclusion where the casing of the solid rocket booster was stiffer at the joints, which allowed a very slight rotation about that joint as the pressure inside built up. coupled with the cold o-rings inflexibility that couldn't keep things sealed and it let the hot gasses out.