| Nombre | apoyo | Revisión | Disponibilidad | Fecha de emisión | Precio | ||
|---|---|---|---|---|---|---|---|
|
PDF |
Inglés |
Vigente |
12/7/2005 |
59,00 € |
|
||
Detalles
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.
Información adicional
| Autor | American Institute of Aeronautics and Astronautics |
|---|---|
| Publicado por | AIAA |
| Tipo de Documento | Norma |
| Número de páginas | 39 |
| Palabra clave | AIAA S-110-2005e |
| ANSI Approved |
