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