EN 16603-32-01:2014
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
30-12-2021
13-08-2014
Foreword
1 Scope
2 Normative references
3 Terms, definitions and
abbreviated terms
4 Principles
5 Fracture control programme
6 Identification and evaluation of PFCI
7 Fracture mechanics analysis
8 Special requirements
9 Material selection
10 Quality assurance and Inspection
11 Reduced fracture control programme
Annex A (informative) - The ESACRACK
software package
Annex B (informative) - References
Bibliography
This ECSS Engineering Standard specifies the fracture control requirements to be imposed on space segments of space systems and their related GSE.The fracture control programme is applicable for space systems and related GSE when required by ECSS-Q-ST-40 or by the NASA document NST 1700.7, incl. ISS addendum.The requirements contained in this Standard, when implemented, also satisfy the fracture control requirements applicable to the NASA STS and ISS as specified in the NASA document NSTS 1700.7 (incl. the ISS Addendum).The NASA nomenclature differs in some cases from that used by ECSS. When STS/ISS-specific requirements and nomenclature are included, they are identified as such.This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
| Committee |
CEN/CLC/JTC 5
|
| DevelopmentNote |
Supersedes EN 14165. (08/2014)
|
| DocumentType |
Standard
|
| PublisherName |
Comite Europeen de Normalisation
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| Standards | Relationship |
| DS EN 16603-32-01 : 2014 | Identical |
| ONORM EN 16603-32-01 : 2014 | Identical |
| PN EN 16603-32-01 : 2014 | Identical |
| I.S. EN 16603-32-01:2014 | Identical |
| BS EN 16603-32-01:2014 | Identical |
| NS EN 16603-32-01 : 2014 | Identical |
| UNI CEI EN 16603-32-01 : 2015 | Identical |
| UNE-EN 16603-32-01:2014 | Identical |
| DIN EN 16603-32-01:2014-10 | Identical |
| NEN EN 16603-32-01 : 2014 | Identical |
| CEI UNI EN 16603-32-01 : 1ED 2016 | Identical |
| NBN EN 16603-32-01 : 2014 | Identical |
| NF EN 16603-32-01 : 2015 | Identical |
| I.S. EN 16602-40:2018 | SPACE PRODUCT ASSURANCE - SAFETY |
| BS EN 16603-32:2014 | Space engineering. Structural general requirements |
| BS EN 16602-40:2018 | Space product assurance. Safety |
| I.S. EN 16603-32-02:2014 | SPACE ENGINEERING - STRUCTURAL DESIGN AND VERIFICATION OF PRESSURIZED HARDWARE |
| BS EN 16603-31-02:2015 | Space engineering. Two-phase heat transport equipment |
| BS EN 16603-34:2014 | Space engineering Environmental control and life support (ECLS) |
| PREN 16603-31-02 : DRAFT 2016 | SPACE ENGINEERING - TWO-PHASE HEAT TRANSPORT EQUIPMENT |
| I.S. EN 16603-31-02:2015 | SPACE ENGINEERING - TWO-PHASE HEAT TRANSPORT EQUIPMENT |
| BS EN 16603-32-02:2014 | Space engineering. Structural design and verification of pressurized hardware |
| I.S. EN 16603-32-08:2016 | SPACE ENGINEERING - MATERIALS |
| I.S. EN 16603-34:2014 | SPACE ENGINEERING - PART 34: ENVIRONMENTAL CONTROL AND LIFE SUPPORT (ECLS) |
| EN 16602-40:2018 | Space product assurance - Safety |
| 16/30336547 DC : 0 | BS EN 16602-70-39 - SPACE PRODUCT ASSURANCE - PART 70-39: WELDING OF METALLIC MATERIALS FOR FLIGHT HARDWARE |
| 16/30352063 DC : 0 | BS EN 16603-31-02 - SPACE ENGINEERING - TWO-PHASE HEAT TRANSPORT EQUIPMENT |
| EN 16603-32-08:2016 | Space engineering - Materials |
| EN 16603-32:2014 | Space engineering - Structural general requirements |
| EN 16603-35-03:2014 | Space engineering - Liquid propulsion for launchers |
| EN 16603-34:2014 | Space engineering - Part 34: Environmental control and life support (ECLS) |
| EN 16603-32-02:2014 | Space engineering - Structural design and verification of pressurized hardware |
| EN 16603-31-02:2015 | Space engineering - Two-phase heat transport equipment |
| I.S. EN 16603-35-03:2014 | SPACE ENGINEERING - LIQUID PROPULSION FOR LAUNCHERS |
| BS EN 16603-35-03:2014 | Space engineering. Liquid propulsion for launchers |
| I.S. EN 16603-32:2014 | SPACE ENGINEERING - STRUCTURAL GENERAL REQUIREMENTS |
| EN ISO 6520-1:2007 | Welding and allied processes - Classification of geometric imperfections in metallic materials - Part 1: Fusion welding (ISO 6520-1:2007) |
| 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 |
| DOT/FAA/AR-MMPDS-01 : 20030131 | METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS) |
| NAS410:2003 | NAS CERTIFICATION & QUALIFICATION OF NONDESTRUCTIVE TEST PERSONNEL |
| EN 16602-70-45:2014 | Space product assurance - Mechanical testing of metallic materials |
| NASA HDBK 5010 : 0 | FRACTURE CONTROL IMPLEMENTATION HANDBOOK FOR PAYLOADS, EXPERIMENTS, AND SIMILAR HARDWARE |
| ISO 3452-2:2013 | Non-destructive testing Penetrant testing Part 2: Testing of penetrant materials |
| ASTM E 426 : 2016 : REDLINE | Standard Practice for Electromagnetic (Eddy Current) Examination of Seamless and Welded Tubular Products, Titanium, Austenitic Stainless Steel and Similar Alloys |
| EN 16601-00-01:2015 | Space systems - Glossary of terms |
| EN 16602-10-09:2014 | Space product assurance - Nonconformance control system |
| SAE AMS 2644 : 2013 | INSPECTION MATERIAL, PENETRANT |
| ASTM E 1444 : 2005 | Standard Practice for Magnetic Particle Testing |
| EN 4179:2017 | Aerospace series - Qualification and approval of personnel for non-destructive testing |
| EN 16603-32:2014 | Space engineering - Structural general requirements |
| MIL-HDBK-6870 Revision B:2012 | NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS |
| EN 16602-20:2014 | Space product assurance - Quality assurance |
| ISO 17659:2002 | Welding — Multilingual terms for welded joints with illustrations |
| EN 16603-32-02:2014 | Space engineering - Structural design and verification of pressurized hardware |
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