BS ISO 16454:2007
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Space systems. Structural design. Stress analysis requirements
Hardcopy , PDF
05-03-2024
English
28-02-2009
Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Requirements
4.1 General
4.2 Basic data
4.3 Analysis methodology and software
4.4 Structural mathematical model
4.5 Structure mathematical model check
4.6 Failure modes
4.7 Critical location analysis
4.8 Determination margins of safety
4.9 Report
Annex A (informative) - Structural mathematical
model check
Covers requirements for the determination of maximum stress and corresponding margin of safety under loading, and defines criteria for static strength failure modes, such as rupture, collapse and detrimental yielding.
Committee |
ACE/68
|
DocumentType |
Standard
|
Pages |
24
|
PublisherName |
British Standards Institution
|
Status |
Superseded
|
SupersededBy |
This International Standard is intended to be used for the determination of the stress/strain distribution and margins of safety in launch vehicles and spacecraft primary structure design. Liquid propellant engine structures, solid propellant engine nozzles and the solid propellant itself are not covered, but liquid propellant tanks, pressure vessels and solid propellant cases are within the scope of this International Standard.
This International Standard provides requirements for the determination of maximum stress and corresponding margin of safety under loading, and defines criteria for static strength failure modes, such as rupture, collapse and detrimental yielding. Critical conditions associated with fatigue, creep and crack growths are not covered. Notwithstanding these limitations in scope, the results of stress calculations based on the requirements of this International Standard are applicable to other critical condition analyses.
In accordance with the requirements of this International Standard, models, methods and procedures for stress determination can also be applied to the displacements and deformation calculations, as well as to the loads definition, applied to substructures and structural members of structures under consideration. When this International Standard is applied, it is assumed that temperature distribution has been determined and is used as input data.
Standards | Relationship |
ISO 16454:2007 | Identical |
ISO 14623:2003 | Space systems - Pressure vessels and pressurized structures — Design and operation |
ISO 14622:2000 | Space systems — Structural design — Loads and induced environment |
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