The Fife said:
I watched through it a couple of times and had to dig a little deeper
https://www.engineering.com/story/the-titan-tragedy-a-deep-dive-into-carbon-fiber-used-for-the-first-time-in-a-submersible
Quote:
A 2017 article in Composite Weekly describes the carbon fiber construction of the Cyclops 2 (later renamed as the Titan) as "alternating placement of prepreg carbon fiber/epoxy unidirectional fabrics in the axial direction" with "wet winding of carbon fiber/epoxy in the hoop direction, for a total of 480 plies."
Building it this way, with no autoclave cure and I'm assuming no meaningful inspection for voids or porosity, FOD, wrinkles, ... is criminally dumb. Go for extra thickness but don't bother with ensuring there's a good bond because who needs that? Probably no attempt to scan the IML or OML for damage between dives either.
I'm surprised it didn't fatigue out before it finally did, but I guess in a way they did their fatigue testing with actual passengers inside and got a data point for what the life limit is.
100% agree. Even more critical when fibers are in compression.
Tanks on space flight vehicles typically have a metal liner that is plastically deformed during testing (autofrettage), preloading the interface and reducing strain extremes, increasing cycle life. The liner also allows for autoclave use to remove air bubbles and voids. Even so, failures STILL occur due to voids between layers.
In the of the Titan, with no autoclave and hand-laid layers, a single void in the exterior and can result in high-pressure water getting pumped further into voids, finding low-pressure pockets to travel into, and gradually cutting into the polymer matrix. 5600 psi water finds a way. Waterjet cutters run at 10X that pressure, but 5600psi still does damage.
This process does weaken the structure, especially with cycling. Combine that with local fiber buckling, stress concentrations, and shearing from water pressure, and it's easy to see how this could fail.
Mike Shaw - Class of '03