Space systems. Structural components and assemblies

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

31-07-2011

Publisher

British Standards Institution

Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Symbols and abbreviated terms
5 Tailoring
6 Requirements
7 Verification of general requirements
8 Special structural items
9 Documentation requirements
10 Data exchange
Annex A (informative) - Recommended best practices for
        structural design
Annex B (informative) - Design requirements verification
        methods
Annex C (informative) - Design requirements verification
        methods
Annex D (informative) - Margin of safety for combined
        loads
Bibliography

Specifies 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.

This International Standard 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. This International Standard, when implemented for a particular space system, will assure high confidence in achieving safe and reliable operation in all phases of its planned mission.

This International Standard 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.

Committee	ACE/68
DevelopmentNote	Supersedes 10/30197714 DC. (07/2011)
DocumentType	Standard
Pages	76
PublisherName	British Standards Institution
Status	Current
Supersedes	10/30197714 DC : 0

Standards	Relationship
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

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BS ISO 10786:2011

Space systems. Structural components and assemblies

Table of Contents

Abstract

Scope

General Product Information

International Equivalents

Standards Referencing This Book

Category

Subcategory