BS EN 14607-7:2004
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 engineering. Mechanical Mechanical parts
Hardcopy , PDF
15-05-2018
English
19-04-2005
Foreword
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
3.1 Terms and definitions
3.2 Abbreviated terms
4 Requirements
4.1 General
4.1.1 Requirements overview
4.1.2 Part classification
4.1.3 Part types
4.1.4 Application
4.2 Mission
4.3 Functionality
4.4 Constraints
4.5 Interface
4.6 Design
4.7 Verification
4.7.1 Product assurance evaluation
4.7.2 Part design verification and sizing requirements
4.7.3 Part qualification
4.7.4 Part acceptance
4.7.5 Summary of the requirement levels
4.7.6 Testing
4.8 Production and manufacturing
4.9 In-service
4.10 Product assurance
4.11 Deliverables
Annex A (informative) Example of a testing matrix
Bibliography
Specifies the requirements applicable to the selection, design, verification and application of mechanical parts to promote the use of high-quality non-critical mechanical parts that achieve robust functionality and satisfy the mission performance requirements.
Committee |
ACE/68
|
DevelopmentNote |
Supersedes 03/301399 DC. (05/2005)
|
DocumentType |
Standard
|
Pages |
18
|
PublisherName |
British Standards Institution
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
EN 14607 Part 7 of Space engineering - Mechanical defines the mechanical engineering requirements for mechanical parts. This document defines the requirements applicable to the selection, design, verification and application of mechanical parts to promote the use of highquality noncritical mechanical parts that achieve robust functionality and satisfy the mission performance requirements. This document defines a pragmatic approach to the selection of parts by the mechanical and design engineer on the basis of their effect on the integrity of the equipment and to streamline the selection of spaceproven rather than non spaceproven parts during the design of a new equipment in order to select the least number of different parts to satisfy the mission requirements. It defines performance, design, test, product assurance and support activity requirements for the use of mechanical parts in space applications. When viewed from the perspective of a specific project context, the requirements defined in this document should be tailored to match the genuine requirements of a particular profile and circumstances of a project. NOTE Tailoring is a process by which individual requirements of specifications, standards and related documents are evaluated, and made applicable to a specific project by selection, and in some exceptional cases, modification of existing or addition of new requirements.
Standards | Relationship |
UNI EN 14607-7 : 2005 | Identical |
NBN EN 14607-7 : 2004 | Identical |
NS EN 14607-7 : 1ED 2004 | Identical |
NF EN 14607-7 : 2004 | Identical |
NEN EN 14607-7 : 2004 | Identical |
DIN EN 14607-7:2006-12 | Identical |
I.S. EN 14607-7:2004 | Identical |
EN 14607-7:2004 | Identical |
MIL-STD-1546 Revision B:1992 | PARTS, MATERIALS, AND PROCESSES CONTROL PROGRAM FOR SPACE AND LAUNCH VEHICLES |
MIL HDBK 5 : G_VOL2 | METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES |
EN 13291-1:1999 | Space product assurance - General requirements - Part 1: Policy and principles |
MIL-STD-410 Revision E:1991 | NONDESTRUCTIVE TESTING PERSONNEL QUALIFICATION AND CERTIFICATION (EDDY CURRENT, LIQUID PENETRANT, MAGNETIC PARTICLE, RADIOGRAPHIC AND ULTRASONIC) |
EN 13291-3:2003 | Space product assurance - General requirements - Part 3: Materials, mechanical parts and processes |
EN 13701:2001 | Space systems - Glossary of terms |
MIL-B-7883 Revision B:1968 | BRAZING OF STEELS, COPPER, COPPER ALLOYS, NICKEL ALLOYS, ALUMINUM AND ALUMINUM ALLOYS |
EN 13290-4:2001 | Space project management - General requirements - Part 4: Project phasing and planning |
EN 13291-2:2003 | Space product assurance - General requirements - Part 2: Quality assurance |
EN 14725:2003 | Space engineering - Verification |
EN 14607-2:2004 | Space engineering - Mechanical - Part 2: Structural |
EN 14607-8:2004 | Space engineering - Mechanical - Part 8: Materials |
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