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Preliminary vibration, acoustic, and shock design and test criteria for components on the SRB, ET, and SSMESpecifications for vibration, acoustic and shock design for components and subassemblies on the External Tank (ET), Solid Rocket Booster (SRB), and Space Shuttle Main Engine (SSME). Included are vibration, acoustic, shock, transportation, handling, and acceptance test requirements and procedures. The space shuttle ET, SRB, and SSME have been divided into zones and subzones. Zones are designated primarily to assist in determining the applicable specifications. A subzone (General Specification) is available for use when the location of the component is known but component design and weight are not well defined. When the location, weight, and mounting configuration of the component are known, specifications for appropriate subzone weight ranges are available. Criteria for some specific components are also presented.
Document ID
19770005171
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Date Acquired
September 3, 2013
Publication Date
November 1, 1976
Subject Category
Space Transportation
Report/Patent Number
NASA-TM-X-64868
Report Number: NASA-TM-X-64868
Accession Number
77N12114
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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