Columbia Space Shuttle Case Study

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INTRODUCTION

This memorandum is a failure analysis report regarding the Space Shuttle Columbia¬, the first space-rated Space Shuttle in NASA’s Orbiter fleet that disintegrated during re-entry during the end of its 28th mission on 1 February 2003 (Columbia Accident Investigation Board [CAIB], 2003, p. 39). The accident, described as a “tragedy” by former President George W. Bush, seized the lives of all seven crew-members aboard and led to a two-year suspension of the Space Shuttle Program (Bush, 2003; CAIB, 2003, p. 209). The following sections of this report outline the events leading up to and during the failure, analyze the reasons behind it, and identify key lessons to apply to future space travel.
DESCRIPTION OF FAILURE

The Shuttle Launch system consists of three components: The Solid Rocket Boosters (SRBs), the External Fuel Tank (ET) and the Orbiter. Several different types of insulating foams cover a large part of the ET, which contains the cryogenic liquid hydrogen and oxygen that fuel the three Space Shuttle Main Engines, to keep the propellants cool and to prevent the formation of ice outside the tank. Approximately 82 seconds into the launch, Columbia was struck by a large piece of foam that had been detached from the
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99). The accident not only led to a revision of current NASA regulations, but also questioned the future of space travel and the presence of the Space Shuttle Program (CAIB, 2003, p. 209). The accident also shed light on the politics involved in NASA funding and the shortcomings of political reform (CAIB, 2003, p. 181). After the accident, NASA introduction of new operational procedures, which included the preparation of an emergency mission for future launches, was, in retrospect, the most significant and crucial change induced by the disaster (CAIB, 2003, p. 173,

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