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AIAA S-110

Space Systems Structures, Structural Components, and Structural Assemblies

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Organization: AIAA
Publication Date: 1 January 2005
Status: active
Page Count: 39
scope:

This document establishes a standard for the design, analysis, material selection and characterization, fabrication, test, and inspection of structural items in space systems, including payloads, spacecraft, upper-stages, and expendable and reusable launch vehicles. This standard, when implemented on a particular space system, will assure high confidence in achieving safe, reliable operation in all phases of the mission. This document applies specifically to all structural items including fracture-critical hardware used in space systems during all phases of the mission-with the following exceptions: adaptive structures, engines, solid rocket nozzles, and thermal protection systems.

Document History

AIAA S-110
January 1, 2005
Space Systems Structures, Structural Components, and Structural Assemblies
This document establishes a standard for the design, analysis, material selection and characterization, fabrication, test, and inspection of structural items in space systems, including payloads,...

References

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