BS EN 16603-32:2014
Current
The latest, up-to-date edition.
Space engineering. Structural general requirements
Hardcopy , PDF
English
31-08-2014
Foreword
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
4 Requirements
Annex A (normative) - Computer aided design
model description and delivery
(CADMDD) - DRD
Annex B (normative) - Design loads (DL) - DRD
Annex C (normative) - Dimensional stability analysis
(DSA) - DRD
Annex D (normative) - Fatigue analysis (FA) - DRD
Annex E (normative) - Fracture control analysis (FCA) - DRD
Annex F (normative) - Fracture control plan - DRD
Annex G (normative) - Fracture control items lists (PFCIL, FCIL
and FLLIL) - DRD
Annex H (normative) - Material and mechanical part allowables
(MMPA) - DRD
Annex I (normative) - Mathematical model description and
delivery (MMDD) - DRD
Annex J (normative) - Modal and dynamic response analysis
(MDRA) - DRD
Annex K (normative) - Stress and strength analysis (SSA) - DRD
Annex L (normative) - Structure alignment budget (SAB) - DRD
Annex M (normative) - Structure buckling (SB) - DRD
Annex N (normative) - Structure mass summary (SMS) - DRD
Annex O (normative) - Test-analysis correlation (TAC) - DRD
Annex P (normative) - Test evaluation (TE) - DRD
Annex Q (normative) - Test prediction (TP) - DRD
Annex R (informative) - Document description list
Annex S (informative) - Effective mass definition
Annex T (informative) - E-32 discipline documents delivery per
review
Bibliography
Describes the mechanical engineering requirements for structural engineering.
| Committee |
ACE/68
|
| DevelopmentNote |
Supersedes BS EN 14607-2. (08/2014)
|
| DocumentType |
Standard
|
| Pages |
140
|
| PublisherName |
British Standards Institution
|
| Status |
Current
|
| Supersedes |
ECSS-E-ST-32C (Space engineering – Structural) defines the mechanical engineering requirements for structural engineering.
This Standard specifies the requirements to be considered in all engineering aspects of structures: requirement definition and specification, design, development, verification, production, in-service and eventual disposal.
The Standard applies to all general structural subsystem aspects of space products including: launch vehicles, transfer vehicles, re-entry vehicles, spacecraft, landing probes and rovers, sounding rockets, payloads and instruments, and structural parts of all subsystems.
This Standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.
| Standards | Relationship |
| EN 16603-32:2014 | Identical |
| DIN EN 16603-32:2014-10 | Equivalent |
| I.S. EN 16603-32:2014 | Equivalent |
| UNE-EN 16603-32:2014 | Equivalent |
| EN 16603-32-01:2014 | Space engineering - Fracture control |
| EN 16602-70-36:2014 | Space product assurance - Material selection for controlling stress-corrosion cracking |
| EN 16602-70:2016 | Space product assurance - Materials, mechanical parts and processes |
| EN 16603-32-11:2014 | Space engineering - Modal survey assessment |
| EN 16601-40:2014 | Space project management - Configuration and information management |
| EN 16603-32-08:2016 | Space engineering - Materials |
| EN 16602-70-37:2014 | Space product assurance - Determination of the susceptibility of metals to stress-corrosion cracking |
| EN 16601-00-01:2015 | Space systems - Glossary of terms |
| EN 16603-32-10:2014 | Space engineering - Structural factors of safety for spaceflight hardware |
| EN 16603-32-03:2014 | Space engineering - Structural finite element models |
| EN 16603-10-03:2014 | Space engineering - Testing |
| EN 16603-32-02:2014 | Space engineering - Structural design and verification of pressurized hardware |
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