Resumen
This International Standard defines the principles used to determine loads and the induced environment during the
service life of a space flight vehicle and its components, taking account of the notions of probability, combined
loads, corresponding safety factors and lifecycle.
Informaciones generales
-
Estado: En desarrolloEtapa: DIS registrado [40.00]
-
Edición: 2Número de páginas: 10
-
Comité Técnico :ISO/TC 20/SC 14ICS :49.140
- RSS actualizaciones
Ciclo de vida
-
Anteriormente
PublicadoISO 14622:2000
-
Ahora
Got a question?
Check out our FAQs
Customer care
+41 22 749 08 88
Opening hours:
Monday to Friday - 09:00-12:00, 14:00-17:00 (UTC+1)