NASA MSFC STD 3676 : 2013
Superseded
Superseded
View Superseded by
DEVELOPMENT OF VIBROACOUSTIC AND SHOCK DESIGN AND TEST CRITERIA
Published date
01-01-2013
Superseded date
08-01-2024
Superseded by
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. INTRODUCTION
5. ENVIRONMENT DEFINITION
6. DESIGN AND VERIFICATION CRITERIA
7. VIBRATION AND SHOCK QUALIFICATION TEST
REQUIREMENTS AND PROCEDURES
8. DESIGN LOADS METHODOLOGY
9. SUMMARY AND CONCLUSIONS
Gives 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.
| DocumentType |
Standard
|
| PublisherName |
National Aeronautics and Space Administration
|
| Status |
Superseded
|
| SupersededBy |
| NASA HDBK 7008 : 2014 | SPACECRAFT DYNAMIC ENVIRONMENTS TESTING |
| NASA MSFC HDBK 3701 : 2015 | MSFC INTEGRATED ENGINEERING PRINCIPLES HANDBOOK |
| NASA STD 7003 : 2011 | PYROSHOCK TEST CRITERIA |
| NASA HDBK 7005 : 2001 | DYNAMIC ENVIRONMENTAL CRITERIA |
| NASA STD 7001 : 2011 | PAYLOAD VIBROACOUSTIC TEST CRITERIA |
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