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BS EN 14607-6:2004

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by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 Pyrotechnics

Available format(s)

Hardcopy , PDF

Superseded date

03-05-2019

Superseded by

BS EN 16603-33-11:2019

Language(s)

English

Published date

19-04-2005

€271.12
Excluding VAT

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 Overview
       4.1.2 Application
       4.1.3 Stability of properties
       4.1.4 Subsystem performance
       4.1.5 Response time
  4.2 Mission
  4.3 Functionality
  4.4 Constraints
       4.4.1 Survival and operational conditions
       4.4.2 Actuators and components
       4.4.3 Mechanical constraints
       4.4.4 Electrical constraints
  4.5 Interface
       4.5.1 Functional
       4.5.2 Internal
       4.5.3 External
  4.6 Design
       4.6.1 Prevention of unintentional function
       4.6.2 Protection
       4.6.3 Monitoring
       4.6.4 Avoidance of single-point failures
       4.6.5 Mechanical design
       4.6.6 Electrical design
       4.6.7 Thermal design
       4.6.8 Specific elements
  4.7 Verification
       4.7.1 General
       4.7.2 Methods
       4.7.3 Essential confirmation
       4.7.4 Routing tests
       4.7.5 End-to-end tests
       4.7.6 Operators
       4.7.7 Subsystem testing
  4.8 Production and manufacturing
       4.8.1 Elements
       4.8.2 Transport and handling
       4.8.3 Facilities
       4.8.4 Electrostatic charge
       4.8.5 Pyrotechnics installation, test and replacement
       4.8.6 Special-purpose aids
       4.8.7 Pyrotechnics hardware tracking
  4.9 In-service
       4.9.1 Launch facilities
       4.9.2 Information feedback
       4.9.3 Launch site procedures
       4.9.4 Commands
       4.9.5 Monitoring
       4.9.6 Recovery
       4.9.7 Disposal of flight equipment
       4.9.8 Final activities
  4.10 Data exchange
       4.10.1 General
       4.10.2 Assembly, integration and verification records
  4.11 Product assurance
       4.11.1 General
       4.11.2 Design and verification
       4.11.3 Dependability
       4.11.4 Safety
       4.11.5 Procurement
       4.11.6 Assembly, integration and testing
       4.11.7 Qualification
       4.11.8 Acceptance
       4.11.9 Post acceptance activities
       4.11.10 Control of pyrotechnics hardware
  4.12 Deliverables
       4.12.1 General
       4.12.2 Documentation
  4.13 Use of the standard to define project requirements
Bibliography
Figures
Tables

Specifies the standards to be applied for the use of pyrotechnics on all spacecraft and other space products including launch vehicles. It addresses the aspects of design, analysis, verification, manufacturing, operations and safety.

Committee
ACE/68
DevelopmentNote
Supersedes 03/301398 DC. (05/2005)
DocumentType
Standard
Pages
36
PublisherName
British Standards Institution
Status
Superseded
SupersededBy
Supersedes

EN 14607 Part 6 of Space engineering - Mechanical defines the requirements for the discipline of pyrotechnics engineering. This part defines the standards to be applied for the use of pyrotechnics on all spacecraft and other space products including launch vehicles. It addresses the aspects of design, analysis, verification, manufacturing, operations and safety. As any pyrotechnic item used for flight can function only once, it can never be fully tested before its crucial mission operation. The required confidence can only be established indirectly by the testing of identical items. Test results and theoretical justification are essential for demonstration of fulfilment of the requirements. The requirement for repeatability shows that product assurance plays a crucial role in support of technical aspects. The failure or unintentional operation of a pyrotechnic item can be catastrophic for the whole mission and life threatening. Specific requirements can exist for the items associated with it. As all pyrotechnic functions are to be treated similarly, collective control needs to be applied in the manner of a subsystem. 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
NEN EN 14607-6 : 2004 Identical
UNI EN 14607-6 : 2005 Identical
NBN EN 14607-6 : 2004 Identical
NS EN 14607-6 : 1ED 2004 Identical
EN 14607-6:2004 Identical
I.S. EN 14607-6:2004 Identical
NF EN 14607-6 : 2004 Identical
DIN EN 14607-6:2006-12 Identical

EN 13291-1:1999 Space product assurance - General requirements - Part 1: Policy and principles
EN 13290-1:1999 Space project management - General requirements - Part 1: Policy and principles
EN 14093:2002 Space project management - Organization and conduct of reviews
EN 13290-5:2001 Space project management - General requirements - Part 5: Configuration management
EN 14824:2003 Space engineering - Testing
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-STD-1576 Base Document:1984 ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS
ISO 14620-1:2002 Space systems Safety requirements Part 1: System safety
EN 14160:2001 Space engineering - Software
DOD-E-83578 Revision A:1987 EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC)
EN ISO 14620-1:2002 Space systems - Safety requirements - Part 1: System safety (ISO 14620-1:2002)
EN 14724:2003 Space project management - Tailoring of space standards
EN 13291-2:2003 Space product assurance - General requirements - Part 2: Quality assurance
EN 14607-2:2004 Space engineering - Mechanical - Part 2: Structural

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