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#11
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Kent Betts wrote: First the engineers were speculating that air and moisture were getting under the foam and getting frozen. Now the idea is that there is stuff under the foam but it is not frozen water from outside, it is cryogenic gas from inside the tank. You misunderstand the report. The cryogenic liquid-gas was liquefied air that seeped by or through the foam. There was no cryo leak. Mike Walsh I don't buy it, because what are the odds that the cryo leak and so forth would occur under the biggest chunk of foam on the tank? I think the foam chunk came off because it was hanging too far out in the airstream and was not of adequate mechanical or aerodynamic design to stay attached at Mach one. The tank attach point insulation is going to get a rework. No mention of it in the press for months. Heh heh....a little amusing that the most direct remedy, fixing the thing that actually caused the accident, is the easiest task on their return to flight to-do list. |
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"Michael Walsh"
You misunderstand the report. The cryogenic liquid-gas was liquefied air that seeped by or through the foam. There was no cryo leak. "We've found out that the bolts and the nuts being applied to actually construct the different areas of the tank ... before you put the insulation on, that any kind of gap in there might be an opportunity for liquid nitrogen or liquid air to form," The article refers to a "different type of cryopumping" but is not explicit as to what this means. I agree that it does not say that there is a cryogenic leak. This was an erroneous supposition on my part upon reading about gaps in the fasteners. It says that gaps around the nuts and bolts provide an opportunity for air and nitrogen to freeze. So at launch time, this frozen stuff heats and expands and does bad stuff to the foam. |
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