Posted on 02/09/2003 5:30:25 PM PST by No Truce With Kings
Corrosion suggested in shuttle crash
Weakened wing may have been vulnerable to impact of debris
By James Oberg
SPECIAL TO MSNBC.COM
IN RECENT DAYS, NASA officials have expressed their frustrated bafflement over the observed debris impact on Columbias left wing. They have repeated studies made during the flight and still come up with results that show the worst-case damage is still far short of a mortal wound that could have prompted the catastrophic failure of the wing. If the falling insulating foam were the triggering event, some additional factor or factors must have been present, they say, to multiply its harmfulness. Accident investigators continue to seek such factors and evaluate them. ONE POSSIBLE EXPLANATION In a two-page memo sent to the NASA space engineering office in Houston, obtained exclusively by MSNBC.com, veteran space shuttle engineer Ray Erikson offers one possible explanation: corrosion of the leading edge spars on the left wing had already so weakened that structure that the small additional damage from the debris was then enough to cause the later failure. In this suggested scenario, the loss of several tiles just behind the left wing leading edge led to significant heating (not catastrophic by itself) that is conducted into the support structure for the leading edge panels. Aluminum is notorious for weakening rapidly at even relatively small temperature increases, and combined with pre-existing corrosion this could have caused a bolt to break free and one leading edge panel to separate. From that point, vehicle loss was inevitable. James Oberg, a former shuttle flight controller, is an author and NBC analyst. Among his books is a history of the U.S.-Russian space alliance titled "Star-Crossed Orbits. |
(Excerpt) Read more at msnbc.com ...
That would be good news. Then again, corrosion could prove to be a big problem anyway if it is from the salt air at the Cape. Who knows where else it could be.
The phenomenon that they are describing where the two metals interact in solution to cause enhanced corrosion is called galvanic corrosion. In order to have this mechanism, there must be a continuous electrolyte (salty water) layer touching both metals. Maybe some part of the wing structure would allow salt spray to condense and run into this area to form a continuous pool, but I don't usually think of these condensation conditions as being ideal for causing galvanic corrosion.
A common problem around bolting is crevice corrosion. This mechanism occurs because a small crevice holds electrolyte and conditions in the crevice become more severe than they are outside the crevice. Salt spray condensing into a crevice can be very aggressive. Galvanic corrosion could be operating within the crevice as well, but the bigger factor might be the crevice.
A problem with inspecting for this problem is that they have to figure out where the salt spray settled on the wings and seeped to the bolts. They may inspect one part of the wing and find no evidence of corrosion at all, but the part of the wing that failed may be full of galvanic or crevice corrosion because that's where the electrolyte solution was. I've seen columns where only a few places suffered cracking but those few places were where the salt spray settled.
In any case, this article is particularly interesting.
WFTR
Bill
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