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Examining the accuracy of the space shuttle support loads using probabilistic analysis techniquesIn order to understand unexpectedly erratic load measurements in the launch-pad supports for the space shuttle, the sensitivities of the load cells in the supports were analyzed using simple probabilistic techniques. NASA engineers use the loads in the shuttle's supports to calculate critical stresses in the shuttle vehicle just before lift-off. The support loads are measured with 'load cells' which are actually structural components of the mobile launch platform (MLP) which have been instrumented with strain gauges. Although these load cells adequately measure vertical loads, the horizontal load measurements have been erratic. The load measurements were simulated in this study using Monte Carlo simulation procedures. The simulation studies showed that the support loads are sensitive to small deviations in strain and calibration. In their current configuration, the load cells will not measure loads with sufficient accuracy to reliably calculate stresses in the shuttle vehicle.
Document ID
19930046994
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Richardson, J.
(Alabama Univ. Tuscaloosa, United States)
Townsend, J. S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 16, 2013
Publication Date
February 1, 1993
Subject Category
Space Transportation
Report/Patent Number
AIAA PAPER 93-1107
Report Number: AIAA PAPER 93-1107
Meeting Information
Meeting: AIAA, AHS, and ASEE, Aerospace Design Conference
Location: Irvine, CA
Country: United States
Start Date: February 16, 1993
End Date: February 19, 1993
Sponsors: AHS, AIAA, ASEE
Accession Number
93A30991
Distribution Limits
Public
Copyright
Other

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