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DEVELOPMENT OF VIBROACOUSTIC AND SHOCK DESIGN AND TEST CRITERIA

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Organization that Developed the Standard
Organization that Developed the Standard
NASA Standard
Document Identifiers
Document Number
MSFC-STD-3676
Version
B
Change Number
0
Document Date
Is Active?
ACTIVE
NASA Organization and Technical Discipline
Responsible NASA Organization
MSFC - Marshall Space Flight Center
Endorsed Standard
Endorsement Details
NASA Core Standard
No
NASA Endorsed Standard Status
Not NASA Endorsed
Mandatory Standard
NASA Mandatory Standard
Not a NASA Mandatory Standard
Document Scope
Document Scope
This document presents the methodology for the development and application of the vibroacoustic and transient design and verification criteria for Marshall Space Flight Center (MSFC) managed launch vehicle and payload hardware.
Keywords
vibroacoustic, transient design, vibration and shock qualification test requirements, design loads methodology
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msfc-std-3676b.pdf (392.62 KB)
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