Space systems — Structural design — Determination of loading levels for static qualification testing of launch vehicles

Available format(s)

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

Superseded date

15-03-2024

Language(s)

English, French

Published date

04-05-2000

Publisher

International Organization for Standardization

This International Standard specifies a procedure for determining the loading level of a qualification test of a launch

vehicle structure and takes into account all the minimum allowable strength characteristics necessary for these

structures.

This International Standard establishes the required resistance necessary for all mass-produced items to comply

with product assurance criteria.

Committee	ISO/TC 20/SC 14
DocumentType	Standard
Pages	4
PublisherName	International Organization for Standardization
Status	Superseded
SupersededBy	ISO 14953:2024
UnderRevision	ISO/FDIS 14953

Standards	Relationship
BS ISO 14953:2000	Identical

ISO 10786:2011	Space systems — Structural components and assemblies
BS ISO 10786:2011	Space systems. Structural components and assemblies
10/30197714 DC : 0	BS ISO 10786 - SPACE SYSTEMS - STRUCTURAL COMPONENTS AND ASSEMBLIES
AIAA S 001 : 1991	TERMINOLOGY FOR SPACE STRUCTURES