The shuttle orbiter Columbia's left wing was increasingly compromised by
the penetration of 2000F reentry plasma starting over the Pacific Ocean
400 mi. off the coast of California, early in the hottest phase of its
disastrous reentry Feb. 1, according to new data released by NASA.
This information provides more detail on sensor readings and when they
occurred relative to the orbiter's ground track during the reentry,
which ended in the loss of Columbia and her seven crewmembers over north
central Texas.
One critical finding is that a breach in the left wing-along its
leading edge, its landing gear door or seals-would had to have occurred
for temperatures in the left wheel well to rise as they did in the final
seconds before breakup began, according to data developed by a NASA
thermal analysis team. The data were provided to the independent
Columbia Accident Investigation Board headed by Adm. (ret.) Harold
Gehman.
The analysis is extremely important because it indicates that missing
thermal tiles alone on the wheel well door would not cause a temperature
rise like that detected before breakup, officials in Houston said.
Sources outside the board noted that it it is increasingly likely the
breach in the wing structure was not specifically in the wheel well
area, although sensors in the wheel well and on the trailing edge of the
wing provided some of the first signs of trouble.
They said the nexus of data from the accident continue to implicate the
impact of insulation from the Lockheed Martin-built external tank on the
left wing as part of a chain of events that could have resulted in a
breach of wing structure.
The Boeing debris impact analysis highlighted both the leading edge of
the wing and an area on the gear door as significant impact areas.
How the breach occurred and its location remain key questions for the
board. But "additional analysis is underway looking at various scenarios
in which a breach of some type, allowing plasma into the wheel well or
elsewhere in the wing could occur," according to a statement from the
board.
It specifically noted that there are no data to support a premature
deployment of the left landing gear, contrary to widespread media
reports late last week.
If debris had damaged the wing's leading edge reinforced carbon-carbon
structures or deeply gouged tiles, allowing hot plasma to penetrate and
erode the underlying aluminum, an increasingly larger path for the
plasma to enter the wing could have been created (AW&ST Feb. 10, p. 22).
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