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Space Shuttle solid rocket booster initial water impact loads and dynamics - Analysis, tests, and flight experienceA series of scale model tests, finite element dynamic response analyses and full scale segment tests have been performed for purposes of developing design criteria for the initial water impact loading conditions applied to the internal stiffener rings located in the aft skirt portion of the Space Shuttle Solid Rocket Booster (SRB). In addition, flight experience has yielded information relative to structural reinforcement requirements. This paper discusses the test and analysis methods and summarizes significant results. It is noted that, although scale model test data are valuable for identifying trends, they have shortcomings concerning definition of full scale design loads criteria. Also, the frequently used static equivalent loads definition approach is not applicable for this type impact loading condition applied to an aft skirt type structure. Various types of ring structural fixes, including the addition of selected types of foam, are presented as well as associated full scale segment test results. Depending on the type and contour shape of the foam, reductions on applied pressures and peak measured strains over 50 percent are noted.
Document ID
19830048640
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kross, D. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Kiefling, L. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Murphy, N. C.
(United Space Boosters, Inc. Huntsville, AL, United States)
Rawls, E. A.
(Chrysler Corp. Michoud, LA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AIAA PAPER 83-0956
Meeting Information
Meeting: Structures, Structural Dynamics and Materials Conference
Location: Lake Tahoe, NV
Start Date: May 2, 1983
End Date: May 4, 1983
Accession Number
83A29858
Distribution Limits
Public
Copyright
Other

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