ISO/CD 14622
u
ISO/CD 14622
85532

Status : Under development

Abstract

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.

General information

  •  : Under development
    : Close of comment period [30.60]
  •  : 2
  • ISO/TC 20/SC 14
    49.140 
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