Conclusions: The hot gases, having flooded the wing interior, quickly heated the upper and lower wing surfaces allowing the aluminum honeycomb facesheets and the wing tiles to debond. The thin-wall aluminum truss tubes would soon collapse and the aerodynamic and structural integrity of the left wing would be effectively destroyed. The forensic evidence is consistent with the observed External Tank foam impact 81 seconds into launch. This is the most probable cause of the damage to the Reinforced Carbon-Carbon. (RCC) leading edge.
Materials and Processes Engineering's Role in the Reconstruction and Failure Analysis of The Space Shuttle Columbia
2005-02-01
Miscellaneous
No indication
English
Space Shuttle Columbia: A Materials Forensic Analysis
NTIS | 2007
|Space Hotels: Civil Engineering's New Frontier
Online Contents | 2002
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