درباره ما
AIAA S-110
Space Systems Structures, Structural Components, and Structural Assemblies
Year: 2005
Abstract: 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.
Show full item record
| contributor author | AIAA - American Institute of Aeronautics and Astronautics | |
| date accessioned | 2017-09-04T16:17:59Z | |
| date available | 2017-09-04T16:17:59Z | |
| date copyright | 2005.01.01 | |
| date issued | 2005 | |
| identifier other | TEIOIBAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsessionid=5419487D58F372296210253C48C0B568/handle/yse/81467 | |
| description abstract | 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. | |
| language | English | |
| title | AIAA S-110 | num |
| title | Space Systems Structures, Structural Components, and Structural Assemblies | en |
| type | standard | |
| page | 39 | |
| status | Active | |
| tree | AIAA - American Institute of Aeronautics and Astronautics:;2005 | |
| contenttype | fulltext |