Space systems — Structural components and assemblies

Available format(s)

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

Language(s)

English

Published date

08-07-2011

Publisher

International Organization for Standardization

ISO 10786:2011 establishes requirements for the design; material selection and characterization; fabrication; testing and inspection of all structural items in space systems, including expendable and reusable launch vehicles, satellites and their payloads. When implemented for a particular space system, it will assure high confidence in achieving safe and reliable operation in all phases of its planned mission.

ISO 10786:2011 applies specifically to all structural items, including fracture-critical hardware used in space systems during all phases of the mission, with the following exceptions: adaptive structures, engines and thermal protection systems.

DevelopmentNote	Supersedes ISO/DIS 10786. (07/2011)
DocumentType	Standard
Pages	65
PublisherName	International Organization for Standardization
Status	Current

Standards	Relationship
BS ISO 10786:2011	Identical

AIAA S 110 : 2005	SPACE SYSTEMS - STRUCTURES, STRUCTURAL COMPONENTS, AND STRUCTURAL ASSEMBLIES
ISO 14954:2005	Space systems — Dynamic and static analysis — Exchange of mathematical models
ISO 24638:2008	Space systems Pressure components and pressure system integration
MIL-STD-1540 Revision D:1999	TEST REQUIREMENTS FOR LAUNCH, UPPER-STAGE, AND SPACE VEHICLES
DOT/FAA/AR-MMPDS-01 : 20030131	METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS)
ASTM E 740 : 2003	Standard Practice for Fracture Testing with Surface-Crack Tension Specimens
ISO 21347:2005	Space systems — Fracture and damage control
ISO 16454:2007	Space systems — Structural design — Stress analysis requirements
ISO 21648:2008	Space systems Flywheel module design and testing
ISO 15864:2004	Space systems General test methods for space craft, subsystems and units
ISO 22010:2007	Space systems — Mass properties control
ISO 24917:2010	Space systems General test requirements for launch vehicles
ISO 14623:2003	Space systems - Pressure vessels and pressurized structures Design and operation
ISO 14953:2000	Space systems — Structural design — Determination of loading levels for static qualification testing of launch vehicles
ISO 14622:2000	Space systems — Structural design — Loads and induced environment