Draft International Standard
ISO/DIS 14622
Space systems — Structural design — Loads and induced environment
Reference number
ISO/DIS 14622
Edition 2
Draft
International Standard
Read sample
u
ISO/DIS 14622
85532
This Draft International Standard is in the enquiry phase with ISO members.
Will replace ISO 14622:2000

ISO/DIS 14622

ISO/DIS 14622
85532
Format
Language
CHF 63
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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

    You can help develop this draft international standard by contacting your national member

    : DIS ballot initiated: 12 weeks [40.20]
  •  : 2
     : 10
  • ISO/TC 20/SC 14
    49.140 
  • RSS updates

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