DIN EN 14607-6-2006 Space engineering - Mechanical - Part 6 Pyrotechnics English version EN 14607-6 2004《航天工程 机械 第6部分 烟火制造 英文版本EN 14607-6 2004》.pdf

《DIN EN 14607-6-2006 Space engineering - Mechanical - Part 6 Pyrotechnics English version EN 14607-6 2004《航天工程 机械 第6部分 烟火制造 英文版本EN 14607-6 2004》.pdf》由会员分享，可在线阅读，更多相关《DIN EN 14607-6-2006 Space engineering - Mechanical - Part 6 Pyrotechnics English version EN 14607-6 2004《航天工程 机械 第6部分 烟火制造 英文版本EN 14607-6 2004》.pdf（35页珍藏版）》请在麦多课文档分享上搜索。

1、Dezember 2006DEUTSCHE NORM Normenausschuss Luft- und Raumfahrt (NL) im DINPreisgruppe 15DIN Deutsches Institut fr Normung e.V. Jede Art der Vervielfltigung, auch auszugsweise, nur mit Genehmigung des DIN Deutsches Institut fr Normung e.V., Berlin, gestattet.ICS 49.140!,c“9645794www.din.deDDIN EN 146

2、07-6Raumfahrttechnik Mechanik Teil 6: Pyrotechnik;Englische Fassung EN 14607-6:2004Space engineering Mechanical Part 6: Pyrotechnics;English version EN 14607-6:2004Ingnierie spatiale Mcanique Partie 6: Pyrotechnie;Version anglaise EN 14607-6:2004Alleinverkauf der Normen durch Beuth Verlag GmbH, 1077

3、2 Berlin www.beuth.deGesamtumfang 35 SeitenDIN EN 14607-6:2006-12 2 Nationales Vorwort Die European Cooperation for Space Standardization (ECSS), eine Einrichtung zur Erstellung eines kohrenten, einheitlichen Normenwerkes zur Anwendung in allen europischen Raumfahrtprojekten, hat am 1996-11-13 vom E

4、uropischen Komitee fr Normung (CEN) das Mandat (M/237) erhalten, fr den CEN-Subsector T02 Aerospace“ Europische Normen (EN) auszuarbeiten. Aufgrund der zwischen ISO/TC 20/SC 14 Raumfahrt“ und ECSS vereinbarten A-Liaison werden die Normungsprogramme dieser Partner abgestimmt und die Abstimmungsregeln

5、 gem Abschnitt 5.2 der Wiener-Vereinbarung angewendet. Die vorliegende Norm EN 14607-6:2004 wurde von CEN/CS T02 auf Basis der ECSS-E-30 erarbeitet. EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 14607-6 August 2004 ICS 49.140 English version Space engineering - Mechanical - Part 6: Pyrotechni

6、cs Ingnierie spatiale - Mcanique - Partie 6: Pyrotechnie Raumfahrttechnik - Mechanik - Teil 6: Pyrotechnik This European Standard was approved by CEN on 27 June 2003. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Sta

7、ndard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the Central Secretariat or to any CEN member. This European Standard exists in three official versions (English, French

8、, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republi

9、c, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATI

10、ON EUROPISCHES KOMITEE FR NORMUNG Management Centre: rue de Stassart, 36 B-1050 Brussels 2004 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 14607-6:2004: EEN 14607-6:2004 (E) 2 Contents page Foreword .4 1 Scope5 2 Normative refer

11、ences5 3 Terms, definitions and abbreviated terms6 3.1 Terms and definitions .6 3.2 Abbreviated terms.7 4 Requirements.10 4.1 General .10 4.1.1 Overview.10 4.1.2 Application .10 4.1.3 Stability of properties10 4.1.4 Subsystem performance.10 4.1.5 Response time.10 4.2 Mission .10 4.3 Functionality 11

12、 4.4 Constraints.11 4.4.1 Survival and operational conditions .11 4.4.2 Actuators and components11 4.4.3 Mechanical constraints.12 4.4.4 Electrical constraints 12 4.5 Interface13 4.5.1 Functional 13 4.5.2 Internal13 4.5.3 External 13 4.6 Design.13 4.6.1 Prevention of unintentional function.13 4.6.2

13、Protection.14 4.6.3 Monitoring 14 4.6.4 Avoidance of single-point failures.14 4.6.5 Mechanical design.14 4.6.6 Electrical design15 4.6.7 Thermal design17 4.6.8 Specific elements 17 4.7 Verification .21 4.7.1 General .21 4.7.2 Methods21 4.7.3 Essential confirmation21 4.7.4 Routing tests21 4.7.5 End-t

14、o-end tests 21 4.7.6 Operators .21 4.7.7 Subsystem testing.21 4.8 Production and manufacturing 21 4.8.1 Elements.21 4.8.2 Transport and handling 22 4.8.3 Facilities .22 4.8.4 Electrostatic charge 22 4.8.5 Pyrotechnics installation, test and replacement22 4.8.6 Special-purpose aids 22 4.8.7 Pyrotechn

15、ics hardware tracking23 4.9 In-service23 4.9.1 Launch facilities 23 EN 14607-6:2004 (E) 3 4.9.2 Information feedback 23 4.9.3 Launch site procedures23 4.9.4 Commands .24 4.9.5 Monitoring 24 4.9.6 Recovery.24 4.9.7 Disposal of flight equipment 24 4.9.8 Final activities24 4.10 Data exchange .24 4.10.1

16、 General .24 4.10.2 Assembly, integration and verification records.25 4.11 Product assurance 25 4.11.1 General .25 4.11.2 Design and verification .25 4.11.3 Dependability .25 4.11.4 Safety26 4.11.5 Procurement.26 4.11.6 Assembly, integration and testing.27 4.11.7 Qualification.27 4.11.8 Acceptance.2

17、9 4.11.9 Post acceptance activities30 4.11.10 Control of pyrotechnics hardware.31 4.12 Deliverables31 4.12.1 General .31 4.12.2 Documentation.31 4.13 Use of the standard to define project requirements32 Bibliography33 Figures Figure 1 Typical pyrotechnic chain and associated items . 9 Tables Table 1

18、 - Document requirements for pyrotechnic subsystem. 32 EN 14607-6:2004 (E) 4 Foreword This document (EN 14607-6:2004) has been prepared by CMC. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by Febr

19、uary 2005, and conflicting national standards shall be withdrawn at the latest by February 2005. It is based on a previous version1) originally prepared by the ECSS Mechanical Engineering Standard Working Group, reviewed by the ECSS Technical Panel and approved by the ECSS Steering Board. The Europe

20、an Cooperation for Space Standardization (ECSS) is a cooperative effort of the European Space Agency, National Space Agencies and European industry associations for the purpose of developing and maintaining common standards. This document is one of the series of space standards intended to be applie

21、d together for the management, engineering and product assurance in space projects and applications. Requirements in this document are defined in terms of what shall be accomplished, rather than in terms of how to organize and perform the necessary work. This allows existing organizational structure

22、s and methods to be applied where they are effective, and for the structures and methods to evolve as necessary without rewriting the standards. EN 14607 Space engineering - Mechanical is published in 8 Parts: Part 1: Thermal control Part 2: Structural Part 3: Mechanisms Part 4: ECLS Part 5: Propuls

23、ion Part 5.1: Liquid and electric propulsion for spacecraft Part 5.2: Solid propulsion for spacecraft, solid and liquid propulsion for launchers Part 6: Pyrotechnics Part 7: Mechanical parts Part 8: Materials According to the CEN/CENELEC Internal Regulations, the national standards organizations of

24、the following countries are bound to implement this European Standard: Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spai

25、n, Sweden, Switzerland and United Kingdom. 1) ECSS-E-30 Part 6A EN 14607-6:2004 (E) 5 1 Scope 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 sp

26、acecraft 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 requir

27、ed 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 technica

28、l 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 i

29、n 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 requirem

30、ents 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. 2 Normative references The following referenced documents are indispensable for the

31、application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 13290-1:1999, Space project management General requirements Part 1: Policy and principles. EN 13290-5:2001,

32、 Space project management General requirements Part 5: Configuration management EN 13291-1:1999, Space product assurance General requirements Part 1: Policy and principles. EN 13291-2:2003, Space product assurance General requirements Part 2: Quality assurance. EN 13291-3:2003, Space product assuran

33、ce General requirements Part 3: Materials, mechanical parts and processes. EN 13701:2001, Space systems Glossary of terms. EN 14093:2002, Space project management Organization and conduct of reviews. EN 14160:2001, Space engineering Software. EN 14607-2:2004, Space engineering Mechanical Part 2: Str

34、uctural. EN 14724:2003, Space project management Tailoring of space standards. EN 14824:2003, Space engineering Testing. EN ISO 14620-1:2002, Space systems Safety requirements Part 1: System safety (ISO 14620-1:2002). ECSS-E-10A, Space engineering System engineering. EN 14607-6:2004 (E) 6 ECSS-E-20A

35、, Space engineering Electrical and electronic. ECSS-Q-30, Space product assurance Dependability. ESA SCC 3401/052, Connectors, electrical, circular, bayonet coupling, scoop-proof, removable crimp contacts. ESA SCC 3401/056, Connectors, electrical, circular, triple-start sel-locking coupling, scoop-p

36、roof, removable crimp contacts. MIL-STD-1576 Issue 31/7/84, Electro-explosive Sub-system Safety Requirements. ST/SG/AC 10/1 Rev. 7, UNO Transport of Dangerous Goods. References to sources of approved lists, procedures and processes can be found in the bibliography. 3 Terms, definitions and abbreviat

37、ed terms 3.1 Terms and definitions For the purposes of this document, the terms and definitions given in EN 13701:2001 and the following apply. 3.1.1 cartridge explosive device designed to produce pressure for performing a mechanical function, i.e. operating a cartridge actuated device such as a pin

38、-puller or cable cutter NOTE 1 A cartridge is called an initiator if it is the first or only explosive element in an explosive chain. NOTE 2 Electrically actuated cartridges are EEDs. 3.1.2 charge quantity of explosive loaded in a cartridge, detonator, or separate container for use in a pyrotechnic

39、device 3.1.3 detonator initiator for high order detonating explosives NOTE Detonators used in space vehicles are generally EEDs, i.e. electrically actuated. 3.1.4 electro-explosive device (EED) explosive initiator that is electrically actuated NOTE 1 The EED is the explosive element used to operate

40、a cartridge actuated device, to initiate an explosive charge, or to ignite a deflagrating material. NOTE 2 Detonators, initiators and cartridges when electrically actuated are EEDs. 3.1.5 initiator first element in an explosive chain that, upon receipt of the proper mechanical or electrical impulse,

41、 produces a deflagrating or detonating action NOTE 1 The deflagrating or detonating action is transmitted to the following elements in the chain. NOTE 2 Initiators can be mechanically actuated, percussion primers, or electrically actuated (EEDs). EN 14607-6:2004 (E) 7 3.1.6 lifetime period over whic

42、h any of the subsystem properties are required to be within defined limits 3.1.7 pyrotechnic actuator mechanism that converts the products of explosion into useful mechanical work 3.1.8 pyrotechnic chain all the elements necessary to supply, operate, support, protect and monitor a pyrotechnic functi

43、on NOTE 1 Software, support equipment, integration, test and launch site facilities and procedures are included in the pyrotechnic chain. NOTE 2 The schematic of a typical pyrotechnic chain is shown in Figure 1. 3.1.9 pyrotechnic component any discrete item containing explosive substance, that is pe

44、rmanently changed as a result of operation 3.1.10 pyrotechnic function any function that uses energy released from explosive substances for its mechanical operation 3.1.11 pyrotechnic subsystem collection of all the pyrotechnic chains on the spacecraft or launcher system, and any on-board computers,

45、 launch operation equipment, ground support and test equipment and all software associated with pyrotechnic functions NOTE Pyrotechnic subsystem is referred to as the subsystem throughout this document. 3.1.12 secondary characteristic any characteristic, other than its primary function, affecting th

46、e capability of an item to meet requirements 3.1.13 sequential firing application of the firing pulses to redundant initiators separated in time 3.1.14 simultaneous firing application of the firing pulse to both redundant initiators at the same instant 3.1.15 sympathetic firing firing of the second

47、of two redundant pyrotechnic devices due to the output of the first 3.2 Abbreviated terms The following abbreviated terms are defined and used within this document. Abbreviation Meaning AIV assembly integration verification DPA destructive physical analysis EED electro-explosive device EGSE electric

48、al ground support equipment EN 14607-6:2004 (E) 8 EMC electromagnetic compatibility ESD electrostatic discharge MGSE mechanical ground support equipment UNO United Nations Organisation TBI through-bulkhead initiator RF radio frequency SRD system requirements document EN 14607-6:2004 (E) 9 Figure 1 T

49、ypical pyrotechnic chain and associated items EN 14607-6:2004 (E) 10 4 Requirements 4.1 General 4.1.1 Overview This document shall be used in addition to any existing standards applicable to spacecraft or launchers and shall be applied in addition to their requirements. This document covers the pyrotechnic subsystem and calls up requirement documents for the subsystem elements. The properties of the electro-explosive device (EED) govern the major part of the behaviour of the whole subsys