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Loads analysis and testing of flight configuration solid rocket motor outer boot ring segmentsThe loads testing on in-house-fabricated flight configuration Solid Rocket Motor (SRM) outer boot ring segments. The tests determined the bending strength and bending stiffness of these beams and showed that they compared well with the hand analysis. The bending stiffness test results compared very well with the finite element data.
Document ID
19900016050
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Ahmed, Rafiq
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1990
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TP-3028
NAS 1.60:3028
Accession Number
90N25366
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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