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Who coined the phrase Rapid Unscheduled Disassembly? Usually simply abbreviated as a RUD, and also sometimes expanded as Rapid Unplanned Disassembly, and being a way of understating that a rocket exploded I saw it attributed recently to Elon Musk, but although he has popularized the phrase among the public, when he mentioned it once in a speech I saw he simply said it is how the engineers on the
tracking - Whats the numeral name of the recently launched Starlink . . . I'd like to track the recently launched Starlink sats that reached a too low orbit due to the Falcon 9 second stage leak and MVac Engine RUD For some reason, if I wanna enter "Launch 11 July 2024" (or 12 July, depending on time zone) in this Starlink tracker, the option doesn't show up
Why did Starship IFT-8 explode again? I've seen pictures of it and videos, but I haven't seen anybody explain what happened Img credit All I know is that the first stage returned and was captured properly, but the 2nd stage didn't ac
Super Heavy explosion, how much TNT equivalent would that be? If the Super Heavy booster explodes, fully loaded, how strong would the blast yield be? How far would the shock wave reach? How does this compare to the N1 RUD's and to other non-nuclear explosio
How does a modern day satellite fall apart in space? 18 How does a modern day satellite fall apart in space? This generic question is answerable They blow up, aka rapid unplanned disassembly (RUD) but due to a large number of causes Or parts fail slowly and the vehicle eventually loses structural integrity There are lots and lots of things that can go wrong on objects in space
Where are the COPVs on Falcon 9s second stage? Data suggests counterintuitive cause " This article mentions "a potential pointer towards the helium pressurization system’s bottles in the Second Stage" or " Composite Overwrap Pressure Vessels " (COPV) Where are these on the upper stage? How likely is it that this could have played a role in the RUD?
What is SpaceX doing differently with Starship to avoid it exploding . . . Perhaps one other thing to note is that the N-1 wasn't even assembled until it reached Baikonur - it had to be shipped overland from the manufacturers, rather than by barge as everyone else does So any kind of integration testing was impossible, especially since the engines could only be fired once
What is the advantage of doing a static test fire before launch? But with the payload in place, RUD during the test fire is hardly a better outcome than RUD during launch I would also expect there to be at least some "bad luck" failure modes that occur only rarely, and are difficult to detect before they do occur (meaning that a test fire before launch effectively just doubles the risk of those failure modes)