Space Shuttle thermal protection system
On February 1, 2003, the Space Shuttle "Columbia" was destroyed on reentry due to a failure of the TPS. The investigation team found and reported that the probable cause of the accident was that during launch, a piece of foam debris punctured an RCC panel on the left wing's leading edge and allowed hot gases from the reentry to enter the wing and disintegrate the wing from within, leading to eventual loss of control and breakup of the shuttle.
Space Shuttle Columbia
"Columbia" was destroyed at about 09:00 EST on February 1, 2003 while re-entering the atmosphere after a 16-day scientific mission. The Columbia Accident Investigation Board determined that a hole was punctured in the leading edge on one of "Columbia's" wings, which was made of a carbon composite. The hole had formed when a piece of insulating foam from the external fuel tank peeled off during the launch 16 days earlier and struck the shuttle's left wing. During the intense heat of re-entry, hot gases penetrated the interior of the wing, likely compromising the hydraulic system and leading to control failure of the control surfaces. The resulting loss of control exposed minimally protected areas of the orbiter to full-entry heating and dynamic pressures that eventually led to vehicle break up.