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Strain gage load measurement on the shuttle orbiterThis paper describes the application of the calibrated strain gage load measurement method to the shuttle orbiter. Descriptions of instrumentation and calibration are included, along with comparisons of measured results with wind tunnel and FLEXSTAB analytical predictions.
Document ID
19830003865
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carter, A. L. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-84898
NAS 1.15:84898
Report Number: NASA-TM-84898
Report Number: NAS 1.15:84898
Meeting Information
Meeting: SESA 1982 Fall Meeting
Location: Hartford, CT
Country: United States
Start Date: November 7, 1982
End Date: November 12, 1982
Accession Number
83N12135
Funding Number(s)
PROJECT: RTOP 506-53-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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