NASA confirms space station cracking a "highest" risk and consequence problem
arstechnica.com
arstechnica.com
One publication I read made a couple of relevant points:
NASA should be careful about privatization and subcontracting, as it replaces NASA top-notch engineers with contract managers and oversight. Most engineers aren't interested in that work, and the skills don't stay sharp.
Also, it said that Gateway, the space station planned to orbit the Moon, is considered the conceptual descendent of ISS.
Much more here: https://nap.nationalacademies.org/cart/download.cgi?record_i...
IMHO NASA should focus on the cutting edge, pushing the frontiers of space and technology. I'm glad they stopped bothering with orbital launch, which they've done for over 60 years - many countries and many private companies can do that now. I'm not sure where ISS falls - LEO is obviously relatively common technology, but habitation in orbit? Space stations orbiting the Moon are the kind of thing where NASA should aim.
What if you worked for a nasa contractor and you got paid quite a bit more than working for nasa?
All aluminum stuff is gonna suffer fatigue problems eventually.
I'm sure NASA has something nicer.
Since this is a docking port connector, they ought to be able to block it off on one side with some sort of temporary airtight seal and measure the direction the air within flows in to gradually narrow down where the leak is.
I get the impression that maybe NASA is avoiding openly discussing the cause of the leak to be nice to roscosmos (because despite all the geopolitical conflict, they're still trying to keep the station running as is for a few more years).
It's a 1 atm difference, so even adhesive tape stuck on the inside would do the trick. Unfortunately, I don't think there is much unexposed hull on the inside and I bet the crack is behind some equipment that isn't trivial to remove (or else it'd have been found years ago by some annoyed astronaut in their off-time).
Detecting from the outside is also complicated, as you'd need to release (and reattach) the thermal blankets to see the actual surface of the module.
Closing the hatch and stopping the use of that docking port seems to be the smart thing to do. Worst case scenario, repressurise, dock the Progress, unload, load it with trash, and close the hatch. I also don't think anyone is considering using this module to boost the station's altitude - I would't put any additional stresses on it anyway.
A better fix would be (believe it or not) drilling holes in it, then sealing it over. This "stop drilling" prevents the crack from growing any larger.
https://old.reddit.com/r/engineering/comments/6bdugb/how_doe...
https://www.upi.com/Archives/1988/05/27/The-recently-imposed...
themoreyouknow.gif
Basically the full workup describes her having a mental breakdown and just making life up there more and more miserable, saying "take me home or I'll escalate" followed by many cycles of not being taken home and escalating. It includes stealing/losing most tools and equipment and "losing them" to the vacuum of space, drilling holes in the space station, and let us diplomatically say... very poor hygiene related to human waste. The astronaut involved basically quit doing any work. Supposedly this ruined the station and basically assured that it be taken offline.
I was an ISS Flight Controller for 6 years and worked in NASA mission planning and the idea that a us astronaut was “losing it in orbit and intentionally drilled a whole” is pretty ridiculous
It’s obvious that the “hole” was some kind of miss by QA on the Russian side on the ground and it’s in Russian media interest currently to spread any unfounded speculation out into the interwebs
Both the Russian Cosmonauts and US Astronauts were eminently professional people hardworking and dependable people and the also ground crews across the world who work night and day operating the station such that no ISS Crewmember should ever deserve to get their names dragged in the mud over this
https://www.snopes.com/fact-check/nasa-astronaut-sabotage-is...
Assuming that NASA is correct about this leak being associated with an interior or exterior weld, what can we learn from the rate of growth of the leak? I assume (with no domain knowledge, seeking enlightenment!) that a leak like this is big enough to reflect a fracture in the weld, and not merely air sneaking past a tiny flaw; and I assume its growth means that the fracture itself is growing, under the combination of load (atmospheric pressure on one side) and cycling (thermal, etc). Is a fracture like this likely to continue to grow in a linear-ish domain, or is there a point where propagation goes non-linear assuming the loads stay constant-ish? Is this even a sane question to ask?
It was a very bad design[1], using substandard material[2] in new and untested ways[3] with poor assembly practices[4]. It was fatally flawed from the start.
1 - Asked about the carbon composite used in Titan’s experimental design, Cameron said, “It’s completely inappropriate for a vessel that sees external pressure.” He went on to say that carbon fiber is very helpful when used for applications subject to internal pressure, like scuba tanks. But, he said, “for something that’s seeing external pressure, all of the advantages of composite material go away and all the disadvantages come into play.”
2 - Another possible "shortcut": https://www.latestly.com/world/titan-submersibles-hull-was-a...
"Expired" bare carbon fiber might be ok; expired prepreg is likely not ok. And I still can't get my head around the apparent mixing of prepreg and wet winding resins in the same laminates.
That article says Boeing has no record of ever selling oceangate composite material. So either he got it for free (Dumpster diving?) or it came from someone else. Maybe some guy in a parking lot: My boss told me to deliver this stuff to Boeing but they wouldn't take it because its expired, I'll sell it to you cheap.
3 - "Thickness, he says, was estimated using micromechanics, and then verified with finite element analysis (FEA).”. >Wonderful. That sort of maybe can work for tension stresses, but can be highly unreliable for compression loading
4 - https://www.youtube.com/watch?v=4PUTbK5AqY8 : >For such a critical joint I see some questionable prep work >in the video. >-Bare hands touching the bond surface. >-Solvent wiping used instead of caustic degreasers. >-Poor wiping technique >-no surface profile/grit blast immediately prior to fixing.
All sources are from commenters on: https://www.eng-tips.com/viewthread.cfm?qid=508005
These kinds of failures tend to be linear until they are not, and the failure mode is catastrophic. If I were in charge I would have already shut off that module on the risk/benefit analysis of catastrophic loss of the station vs. not being able to evacuate as quickly in a less catastrophic emergency. Maybe they are worried they won't be able to get the hatch open again if they can't equalize the pressure again?
For historical reference, consider Aloha Airlines Flight 243[1].
Well note that they currently keep the hatch to the docking port closed unless they're using it, so that presumably mitigates some of the risk (assuming the leak is confined to that location). Not using the whole Zvezda module itself would be more or less impossible from my understanding.
If they decided to stop using that dock port at all then I think that complicates planning and makes everything overall riskier, so while it wouldn't be a disaster to do there's still risk you have to weigh.
Welds fail for multiple reasons - heating too fast, cooling too fast, material defects, human error, equipment issues, oxidation. The best human welder will still have some variance in their weld even if they lay a perfect bead.
Once a weld begins to fail, under normal conditions (vibration, stress, etc), it will slowly get worse, but that can also mean deformation around the weld or even sometimes shearing right next to your weld. The article doesn't mention that the growth has been linear only that it is increasing. I expect that the leak is increasing over time in a non-linear fashion as force is applied to the weak area and metal continues to separate and/or shear. Still, 3.7 pounds of atmosphere a day is a very slow leak (relatively), a few bike tires a day.
I'd just paint over all the welds and be happy until it unseals itself again.
It depends on so much that we don't know from the article.
A mental subprocesses spawned to predict whether the cracking was _of_ the systems on the station—possibly inspired by that movie trailer I saw for the thriller about a new cold war in space after a nuclear war—or _from_ the space station, by bored occupants, either of their own systems or of some system they interact with on the ground.
A bit deflated by the reality, tbh.