1272305

AIAA S-110-2005e

Space Systems - Structures, Structural Components, and Structural Assemblies

standard by American Institute of Aeronautics and Astronautics , 07/12/2005

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Full Description

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.
 

Product Details

Published:
07/12/2005
ANSI:
ANSI Approved
Number of Pages:
39
File Size:
1 file , 570 KB
Note:
This product is unavailable in Ukraine, Russia, Belarus