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
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Estado: En desarrolloEtapa: Texto final recibido o FDIS registrado para su aprobación formal [50.00]
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Edición: 2
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Comité Técnico :ISO/TC 20/SC 14ICS :49.140
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Ciclo de vida
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Anteriormente
PublicadoISO 14622:2000
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Ahora