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Modal analysis and dynamic stresses for acoustically excited shuttle insulation tilesImprovements and extensions to the RESIST computer program developed for determining the normalized modal stress response of shuttle insulation tiles are described. The new version of RESIST can accommodate primary structure panels with closed-cell stringers, in addition to the capability for treating open-cell stringers. In addition, the present version of RESIST numerically solves vibration problems several times faster than its predecessor. A new digital computer program, titled ARREST (Acoustic Response of Reusable Shuttle Tiles) is also described. Starting with modal information contained on output tapes from RESIST computer runs, ARREST determines RMS stresses, deflections and accelerations of shuttle panels with reusable surface insulation tiles. Both programs are applicable to stringer stiffened structural panels with or without reusable surface insulation titles.
Document ID
19760013104
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ojalvo, I. U.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Ogilvie, P. L.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-144958
Report Number: NASA-CR-144958
Accession Number
76N20192
Funding Number(s)
CONTRACT_GRANT: NAS1-10635
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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