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STS-1 Forward RCS Oxidizer Tank Subsystem Failure AssessmentThe launch of the Space Shuttle Columbia on STS-1 marked the beginning of a new
era in American spaceflight. It was the only crewed first flight of a launch vehicle to date,
and was also the first crewed system to use large solid rockets as primary propulsion. A
potential disaster was narrowly averted at liftoff when an ignition overpressure pulse swept
up the Shuttle stack. The frequency of this transient shock wave exceeded pre-launch
predictions, and resulted in high, alternating normal accelerations along the length of the
vehicle. Among the results of this unexpected loading was failure of an oxidizer tank
support strut in the orbiter’s forward reaction control system module, which could have led
to loss of the mission, crew, and vehicle. This particular incident is investigated in more
detail using classical structural mechanics, and the results are discussed to provide
additional insight.
Document ID
20205007677
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
K Chauncey Wu
(Langley Research Center Hampton, Virginia, United States)
John J Zipay
(Johnson Space Center Houston, Texas, United States)
Date Acquired
September 16, 2020
Subject Category
Structural Mechanics
Meeting Information
Meeting: 2021 Science and Technology (SciTech) Forum and Exposition
Location: Virtual
Country: US
Start Date: January 11, 2021
End Date: January 15, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 062285.01.02.09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Space Shuttle
Buckling
Failure Analysis
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