BS ISO 10786:2011
Current
The latest, up-to-date edition.
Space systems. Structural components and assemblies
Hardcopy , PDF
English
31-07-2011
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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.
| Committee |
ACE/68
|
| DevelopmentNote |
Supersedes 10/30197714 DC. (07/2011)
|
| DocumentType |
Standard
|
| Pages |
76
|
| PublisherName |
British Standards Institution
|
| Status |
Current
|
| Supersedes |
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.
| 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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