Elon Musk: Faulty Strut May Have Led To Falcon 9 Launch Failure
garyisabusyguy writes: This Forbes article provides the best analysis of the loss of the last Falcon 9 mission based on information released by Elon Musk to reporters. Highlights include:
- 1. Sound triangulation led them to identify a strut holding helium tank as root cause where the falling helium tank pinched a line causing overpressure in the LOX tank.
- 2. The failure occurred at 2,000 pounds of force, and the struts were rated at 10,000 pounds of force. They initially dismissed this as a cause until sounds triangulation pointed back to the strut
- 3. Further testing of struts in stock found one that failed at 2,000 pounds of force, with further analysis identifying poor grain structure in the metal, which caused weakness
- 4. It will be months before the next launch while SpaceX goes over procurement and QA processes all struts and bolts, and re-assesses any "near misses" with Air Force and NASA
- 5. Next launch will include failure mode software, which will allow recovery of the Dragon module during loss of the launch vehicle since they determined that it could have saved the Dragon module in this lost mission
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Now THAT is how you summarize.
So after weeks of investigation it turns out it's a failure mode that even the most amateur of KSP players recognize.
They should have added a lot more of them, clearly. It's not like struts have any mass.
Sell them faulty metal.
Or faulty parts made of metal.
It's just a thought, but would a competitor stoop to that? Even if not now, at some point in the future?
I'll see your senator, and I'll raise you two judges.
You can test random struts, but you can't test ALL struts or you're left with no struts. Sounds like they didn't test the right ones is all.
Quite true, but there are OTHER ways of figuring out the strength of the part other than testing them to failure or causing damage to the parts. Some of these methods are quite expensive, but effective. How you get a one part that's 1/4th the strength the design requires through a manufacturing process, onto a flight ready hardware assembly and not know it says serious problems lurk within. Seems Space-X has some defects in it's quality assurance processes, and that should scare you more than this one launch failure. They are playing way too fast and loose with quality and I'd be very worried about their efforts towards getting "human" rated are not going well.
This was a structural failure. A failure that can likely be traced to a part that was too weak for the designed loads. This isn't a DESIGN failure, it's a QUALITY failure, and that puts the whole program into question. What has to happen now is that the whole QA process needs to be revisited and revamped to prevent structural components from sneaking though which are not strong enough to do what they are designed to. THEN you have to go though your whole stock of parts, sub assemblies, and flight ready assemblies and figure out what you can verify as trustworthy using your NEW QA process, throw out the rest and order, assemble and test replacements.
This isn't an easy or quick fix...
Then there is the whole, our supplier lied to us, approach, which will be quicker to deal with, but only because you just have to obtain a batch of replacement struts, fully tested and verified, replace all existing hardware that used the old ones by either reworking the assemblies or building new ones that have the new parts.....
I'm guessing Space-X will opt for the latter in public, but unless they sue the supplier for damages, the problem really is the former, which scares me..
"File to fit, pound to insert, paint to match" - Aircraft Maintenance 101
Yep. Once you have thousands of parts all designed to trade off as much strength for weight reduction as possible it doesn't take much of a manufacturing hiccup to cause an expensive "excursion". Vendors end up having to rigorously test every widget, and custom design it just for you.
Before long $10k each for a batch of a half dozen toilets seat that are space rated to not outgas funny chemicals that foul optics, handles 10g's, has 6 sigma of de-rating for the bolt hole strength, weighs under 500g, and is non-flammable starts sounding like a deal.
Pilot wouldn't have needed to. Dragon 2 has automatic abort capabilities (even when unmanned). It would have separated from the second stage - probably firing its SuperDraco thrusters - and then automatically deployed parachutes once it was a safe distance away.
Dragon 1 doesn't have the SuperDracos (only the much smaller Draco attitude control thrusters) so it wouldn't have been able to put as much distance between itself and the booster, but from the video and the telemetry it looks like the capsule survived the (accidental) separation anyhow. It could have deployed its parachutes and probably survived the landing, but it wasn't programmed to do so. They have added it to the Dragon 1 programming now though.
Failures that occur high enough to land under parachutes, slow enough to get away from the inevitable explosion without heavy rockets, and early enough in flight that there's no time to manually enable the landing sequence are... really, really rare in rocketry. Usually you either fail at liftoff (see Orbital's last attempt to launch Antares), fail rapidly and catastrophically during liftoff (any number of examples), or fail once in orbit (often, though not always, at stage separation). In orbit you have time to make a decision and send orders. On the launchpad you can't land safely (without abort rockets). In midair you *usually* can't get away in time (without abort rockets). This was an exception to the "in midair" usual failure case; there were nine seconds from beginning of the failure to loss of vehicle, and in fact the capsule had already tumbled free (and probably *could* have used its ACS thrusters to put some extra distance between itself and the booster.
One thought, though: what about, in the case of a pre-separation second-stage failure, executing MECO 1 (Main Engine Cut Off, when the Falcon 9 first stage kills its rockets) early and doing an emergency stage separation? Normally there's no point - the first stage on most launch vehicles has no purpose if the launch fails and nowhere to go even if it separates safely - but the Falcon 9 first stage is designed for reusability. Emergency MECO, separate the stages, use the ACS and/or grid fins to steer clear of the second stage, and then fire up the main engines again and aim for the droneship or other landing pad. You'd need to be quick about it, and it might still not work, but if it does you've saved a booster worth $70,000,000 USD. Well, that and demonstrated the first successful first stage recovery ever, but assuming that becomes as routine as Musk wants it to be...
Actually, it would have been super cool if the first successful recovery of the first stage had been an emergency abort!
There's no place I could be, since I've found Serenity...