CRS-7 Investigation Update
spacex.com
spacex.com
It's great they're publicly releasing their preliminary findings, but they're also practically patting themselves on the back while doing it. It reads more smarmy than refreshing.
Huh. So the strut was way over-engineered for the load and still failed, likely due to a hidden mechanical flaw. Would that make more sense to use a large number of smaller struts then, such that a failure of one or two would be less problematic? You can even test the design for it - make sure the rocket is still working when certain number of struts fail. The assembly cost would certainly rise, but the current design seems to be not sufficiently redundant.
If you add triple-redundancy to all the mechanical elements you build a rocket that probably can't fly - which is certainly very safe, but maybe not so very useful.
I'd guess the problem has more to do with insufficient testing than insufficient design. It's likely the initial batch was easily up to spec, then there was little or no testing of further batches.
Easy mistake, IMO. If you think about the number of critical components, re-testing everything before every flight would be a huge and very expensive job.
I wonder if SpaceX are going to do less business with the strut supplier in future.
I think there is a more succinct and straightforward, if not completely accurate, summary of events: A strut broke and smashed into the helium system, and released helium pressure blew the tank apart.
If you're talking to average people, yes, your way of wording it would be more efficient.
However in certain domains accuracy is key, so one tries to communicate with as much detail as possible. In order to achieve this without being hyper-verbose, one uses an established set of vocabulary, whose subtle and detailed meaning is well-understood and common in that industry. That may make it sound strange to outsiders, but minimizes the risk for misunderstandings and lack of clarity amongst peers.
The SpaceX description is a little vague about the plumbing, I'd like to know more about that - is it an on off vale that opens and closes under command of the flight computer to maintain pressure, or is it a modulated valve that is controlled by a PID loop or the like.
What's ambitious is when they say they plan to complete their original 2015 launch manifest in 2015. That made me sit up and take notice.