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Loads and Structural Dynamics Requirements for Spaceflight Hardware

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SUNS Notification Type
Revision
Organization that Developed the Standard
Organization that Developed the Standard
NASA Standard
Document Identifiers
Document Number
JSC-65829
Version
B
Change Number
0
Document Date
Is Active?
ACTIVE
NASA Organization and Technical Discipline
Responsible NASA Organization
JSC - Johnson Space 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 is intended to cover analyses representing all phases of spaceflight hardware life
cycles, including pre-flight, post-flight, and abort activities. The requirements herein represent
the minimum set of conditions necessary to ensure proper identification of bounding loads and
loading conditions and, in turn, contribute to a structural design solution which is adequate to
maintain structural integrity and the required degree of functionality during all phases of the
expected hardware life cycle. However, this document cannot cover all possible designs and
situations, so it is not a substitute for sound engineering judgment in design, analysis, and test.
The definition of natural environments to be used for design loads derivation is out of scope of
this document.
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JSC-65829-Loads-Dyn_Req_for_SF_Hardware-RevB_signed_page2_footer_corrected_0.pdf (1.22 MB)
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JSC-65829-Loads-Dyn_Req_for_SF_Hardware-RevB_signed_page2_footer_corrected.pdf (1.22 MB)
Additional Comments
This document has been reviewed for Proprietary, SBU, and Export Control (ITAR/EAR) and has been
determined to be non-sensitive. It has been approved for public release via the NASA Scientific and Technical
Information (STI) Process DAA 20240003625.
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