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Ctrl+shift+i in Chrome, Console, you may see something like "blocked by client".


"... all experience hath shewn, that mankind are more disposed to suffer, while evils are sufferable, than to right themselves by abolishing the forms to which they are accustomed."

https://en.wikipedia.org/wiki/United_States_Declaration_of_I...


Will need to wait until the year 2375 for the next renaissance: https://vignette.wikia.nocookie.net/memoryalpha/images/5/54/...


It all depends on how an engine fails. A failure to provide thrust is survivable with more engines. But a vulnerability that causes a fuel line to go boom, taking out the whole rocket, is made more likely by having more engines.


IIRC, the engines in the Falcon 9 are pretty well separated from each other, such that even a catastrophic failure of one engine is survivable by the rest. Indeed, that seems to be what happened the one time an engine did fail (albeit on a very early version of the Falcon 9 with the "square" engine layout): https://www.youtube.com/watch?v=dvTIh96otDw


It is not an explosion. From the first comment:

Engine didn't explode, it detected an anomaly and shut itself down. Here's spacex's statement concerning the event-

"Approximately one minute and 19 seconds into last night's launch, the Falcon 9 rocket detected an anomaly on one first stage engine. Initial data suggests that one of the rocket's nine Merlin engines, Engine 1, lost pressure suddenly and an engine shutdown command was issued. We know the engine did not explode, because we continued to receive data from it. Panels designed to relieve pressure within the engine bay were ejected to protect the stage and other engines."


> Panels designed to relieve pressure within the engine bay were ejected to protect the stage and other engines.

Does anyone have details on this? I'm just curious how these work because it sounds fascinating.


I believe that was actually the reason why they moved to a "round" configuration.

They realized that the "corner" engines were doing more work, and if one of them failed it caused larger issues than they were expecting.

However in the "round" layout, all of the engines are doing the same amount of work and have a similar amount of control over the rocket, so one failing can be more easily compensated for by the surrounding engines.


I believe it was not due to this but due to mass savings. The square grid layout uses more material and in a less symmetric way too.


I believe a leak in a fuel line (even a dissection) would need oxygen to cause an explosion rather than failure, and would not be enough force to cause a structural failure. The fuel isn't under extreme pressure, else those pumps wouldn't be needed, and Pogo effects wouldn't have been a problem.


Exactly - engine-out failures are far more common than boom failures, so it makes sense to have lots of small engines.

The Soviet N-1 failures had more to do with rushed, shoddy engineering in a desperate attempt to catch up to Apollo.


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