Space systems — Structural design — Loads and induced environment

Available format(s)

Hardcopy , PDF 1 User , PDF 3 Users , PDF 5 Users , PDF 9 Users

Language(s)

English, French

Published date

21-12-2000

Publisher

International Organization for Standardization

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.

DocumentType	Standard
Pages	9
PublisherName	International Organization for Standardization
Status	Current

ISO 10786:2011	Space systems — Structural components and assemblies
ISO 16454:2007	Space systems — Structural design — Stress analysis requirements
BS ISO 10786:2011	Space systems. Structural components and assemblies
10/30197714 DC : 0	BS ISO 10786 - SPACE SYSTEMS - STRUCTURAL COMPONENTS AND ASSEMBLIES
BS ISO 16454:2007	Space systems. Structural design. Stress analysis requirements
05/30099159 DC : DRAFT FEB 2005	ISO 16454 - SPACE SYSTEMS - STRUCTURAL DESIGN - STRESS ANALYSIS REQUIREMENTS