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Water impact testing of a filament wound caseA lightweight Filament Wound Case (FWC) Solid Rocket Booster (SRB) is being developed by NASA to increase the payload capability of the space shuttle. As with the steel boosters, the current plan is to recover the FWC SRB's after they impact the ocean at 65 to 85 ft/sec. As the boosters enter the ocean (nozzle first) the water moves away from the vehicle creating a cavity, which then collapses on the vehicle, and results in a significant loading event. To understand this loading event, tests were conducted on a quarter scale FWC model to measure cavity collapse pressure distributions, deflected shape and the effects of end conditions and pressure scaling.
Document ID
19860007182
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Schmidt, A. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Kross, D. A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1985
Publication Information
Publication: Shock and Vibration Information Center The Shock and Vibration Bulletin 55, Part 2
Subject Category
Structural Mechanics
Accession Number
86N16652
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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