1、BSI Standards PublicationBS EN 16603-32-02:2014Space engineering Structuraldesign and verification ofpressurized hardwareBS EN 16603-32-02:2014 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN16603-32-02:2014.The UK participation in its preparation was entrusted
2、to TechnicalCommittee ACE/68, Space systems and operations.A list of organizations represented on this committee can beobtained on request to its secretary.This publication does not purport to include all the necessaryprovisions of a contract. Users are responsible for its correctapplication. The Br
3、itish Standards Institution 2014. Published by BSI StandardsLimited 2014ISBN 978 0 580 83981 8ICS 49.140Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStandards Policy and Strategy Committee on 31 August 2
4、014.Amendments issued since publicationDate Text affectedBS EN 16603-32-02:2014EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 16603-32-02 August 2014 ICS 49.140 English version Space engineering - Structural design and verification of pressurized hardware Ingnierie spatiale - Conception struct
5、urelle et vrification des elements pressurises Raumfahrttechnik - Strukturdesign und -verifikation von druckbeaufschlagten Teilen This European Standard was approved by CEN on 10 February 2014. CEN and CENELEC members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the
6、conditions for giving this European Standard 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 CEN-CENELEC Management Centre or to any CEN and CENELEC member. This Europea
7、n Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN and CENELEC member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions. CEN a
8、nd CENELEC members are the national standards bodies and national electrotechnical committees of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania
9、, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brussels 2014 CEN/CENELEC All rights of exploitation in any form and by any means reserved worldwide
10、 for CEN national Members and for CENELEC Members. Ref. No. EN 16603-32-02:2014 EBS EN 16603-32-02:2014EN 16603-32-02:2014 (E) 2 Table of contents Foreword 5 1 Scope . 6 2 Normative references . 7 3 Terms, definitions, and abbreviated terms . 8 3.1 Terms from other standards 8 3.2 Terms specific to
11、the present standard . 8 3.3 Abbreviated terms. 14 3.4 Symbols 15 4 General requirements. 16 4.1 Overview 16 4.1.1 Content . 16 4.1.2 Categories of pressurized hardware 16 4.2 General . 17 4.2.1 Leak tightness . 17 4.2.2 Classification of fracture critical parts 17 4.2.3 Operation and maintenance 18
12、 4.2.4 Service life extension, reactivation and re-acceptance 20 4.3 Pressure vessels 21 4.3.1 Factors of safety . 21 4.3.2 Metallic pressure vessels 22 4.3.3 COPV with metallic liner 25 4.3.4 COPV with homogeneous non metallic liner and CPV 29 4.4 Pressurized structures 33 4.4.1 Factors of safety .
13、 33 4.4.2 Metallic pressurized structures 34 4.4.3 COPS with metallic liner 36 4.4.4 COPS with homogeneous non metallic liner and CPS 39 4.5 Pressure components . 43 4.5.1 Metallic pressure components . 43 BS EN 16603-32-02:2014EN 16603-32-02:2014 (E) 3 4.5.2 COPC with metallic liner 45 4.5.3 COPC w
14、ith homogeneous non metallic liner . 48 4.6 Special pressurized equipment . 51 4.6.1 Metallic special pressurized equipment . 51 4.6.2 COSPE with metallic liner . 58 4.6.3 COSPE with homogeneous non metallic liner . 61 5 Specific requirements 65 5.1 Overview 65 5.2 Structural engineering . 65 5.3 Fa
15、ilure mode demonstration . 66 5.3.1 General . 66 5.3.2 Demonstration of LBB by analysis . 67 5.3.3 Demonstration of LBB by test using coupons 68 5.3.4 Demonstration of LBB by test using full-scale article . 68 5.3.5 Report of LBB demonstration 69 5.4 Qualification tests . 70 5.4.1 General . 70 5.4.2
16、 Proof pressure test 70 5.4.3 Leak test . 71 5.4.4 Vibration test . 71 5.4.5 Pressure cycling test . 71 5.4.6 Design burst pressure test 71 5.4.7 Burst test . 71 5.5 Acceptance tests 72 5.5.1 General . 72 5.5.2 Proof pressure test 72 5.5.3 Leak test . 72 5.6 Composite over-wrap material characteriza
17、tion 73 5.7 Inspection . 73 5.7.1 General . 73 5.7.2 Inspection techniques for composite over-wraps and composites . 74 Bibliography . 75 Figures Figure 4-1: Breakdown of PH types covered by this Standard 16 Figure 4-2: Flowchart describing PH classifications covered by this Standard 17 BS EN 16603-
18、32-02:2014EN 16603-32-02:2014 (E) 4 Figure 4-3: Development approach of MPV 23 Figure 4-4: Development approach of COPV with metallic liner 28 Figure 4-5: Development approach of COPV with homogeneous non metallic liner and CPV . 32 Figure 4-6: Development approach of MPS 35 Figure 4-7: Development
19、approach of COPS with metallic liner 39 Figure 4-8: Development approach of COPS with homogeneous non metallic liner and CPS . 42 Figure 4-9: Development approach of MPC 45 Figure 4-10: Development approach of sealed containers 54 Figure 4-11: Development approach of cryostats (or Dewars) 55 Figure
20、4-12: Development approach of heat pipes . 56 Figure 4-13: Development approach of hazardous fluid containers 57 Tables Table 4-1: Factors of safety for PV (unmanned and manned missions) 22 Table 4-2: Factors of safety for PS (unmanned mission) 33 Table 4-3: Factors of safety for PS (manned mission)
21、 33 Table 4-4: Factors of safety for manned modules . 33 Table 4-5: Factors of safety for MPC (unmanned and manned missions) . 43 Table 4-6: Factors of safety for COPC with metallic liner (unmanned and manned missions) 46 Table 4-7: Factors of safety for COPC with homogeneous non metallic liner (unm
22、anned and manned missions) . 49 Table 4-8: Factors of safety for MSPE (unmanned and manned missions). 52 Table 4-9: Factors of safety for COSPE with metallic liner (unmanned and manned missions) 59 Table 4-10: Factors of safety for COSPE with homogeneous non metallic liner (unmanned and manned missi
23、ons) 61 BS EN 16603-32-02:2014EN 16603-32-02:2014 (E) 5 Foreword This document (EN 16603-32-02:2014) has been prepared by Technical Committee CEN/CLC/TC 5 “Space”, the secretariat of which is held by DIN. This standard (EN 16603-32-02:2014) originates from ECSS-E-ST-32-02C Rev. 1. This European Stan
24、dard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by February 2015, and conflicting national standards shall be withdrawn at the latest by February 2015. Attention is drawn to the possibility that some of the elements o
25、f this document may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. This document has been developed to cover specifically space systems and has therefore precedence over any EN covering the same scope but with a wider
26、domain of applicability (e.g. : aerospace). According to the CEN-CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former
27、 Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 16603-32-02:2014EN 16603-32-02:2014 (
28、E) 6 1 Scope This Standard defines the structural design verification of metallic and non-metallic pressurized hardware which includes pressure vessels, pressurized structures, pressure components (such as valves, pumps, lines, fittings, and hoses), and special pressurized equipment (e.g. batteries,
29、 heat pipes, cryostats, sealed containers, hazardous fluids container). External supports and structural interfaces of pressurized hardware are not covered by this standard. Solid propellant motor cases are not covered by this standard. Objectives of the associated verification process are primarily
30、 to demonstrate the qualification of design and performance, as meeting all specified requirements, and to ensure that the flight hardware is free from workmanship defects and acceptable for flight. This Standard applies to all space products and in particular to launch vehicles, transfer vehicles,
31、re-entry vehicles, spacecraft, space station, landing probes and rovers, sounding rockets, payloads and instruments. This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00. BS EN 16603-32-02:2014EN 16603-32-02:2014 (E) 7 2 N
32、ormative references The following normative documents contain provisions which, through reference in this text, constitute provisions of this ECSS Standard. For dated references, subsequent amendments to, or revision of any of these publications, do not apply. However, parties to agreements based on
33、 this ECSS Standard are encouraged to investigate the possibility of applying the more recent editions of the normative documents indicated below. For undated references, the latest edition of the publication referred to applies. EN reference Reference in text Title EN 16601-00-01 ECSS-S-ST-00-01 EC
34、SS system Glossary of terms EN 16603-10-02 ECSS-E-ST-10-02 Space engineering Verification EN 16603-10-03 ECSS-E-ST-10-03 Space engineering Testing EN 16603-32 ECSS-E-ST-32 Space engineering Structural general requirements EN 16603-32-01 ECSS-E-ST-32-01 Space engineering Fracture control EN 16603-32-
35、08 ECSS-E-ST-32-08 Space engineering Materials EN 16603-32-10 ECSS-E-ST-32-10 Space engineering Reliability based mechanical factors of safety EN 16602-20 ECSS-Q-ST-20 Space product assurance Quality assurance EN 16602-70 ECSS-Q-ST-70 Space product assurance Materials, mechanical parts and processes
36、 BS EN 16603-32-02:2014EN 16603-32-02:2014 (E) 8 3 Terms, definitions, and abbreviated terms 3.1 Terms from other standards For the purpose of this Standard, the terms and definitions from ECSS-S-ST-00-01, ECSS-E-ST-32, and ECSS-E-ST-32-01 apply. 3.2 Terms specific to the present standard 3.2.1 auto
37、frettage vessel sizing operation where pressure driven deflection is used to plastically yield the metal liner into the overlying composite in order to induce initial compressive stress states in the metal liner NOTE Autofrettage is considered to be part of the manufacturing process and is conducted
38、 prior to acceptance test. 3.2.2 boss zone of a pressure vessel or a pressurized structure ensuring functional interfaces (e.g. fluid connections and mechanical interfaces) of the hardware with the pressurized system 3.2.3 burst factor (jburst) multiplying factor applied to the maximum design pressu
39、re (MDP), to obtain the design burst pressure NOTE The burst factor corresponds to an ultimate factor of safety. 3.2.4 burst pressure pressure level at which collapse, rupture or unstable fracture of the pressurized hardware occurs 3.2.5 composite over-wrap layers of fibre-based composite material a
40、pplied onto a liner, sustaining significant pressure and environmental loads BS EN 16603-32-02:2014EN 16603-32-02:2014 (E) 9 3.2.6 composite over-wrapped pressure vessel (COPV) pressure vessel with a fibre-based composite structure fully or partially encapsulating a liner NOTE For example: the liner
41、 can be metallic or not. the liner ensures the leak tightness of the vessel. 3.2.7 composite over-wrapped pressurized component (COPC) pressurized component with a fibre-based composite system fully or partially encapsulating a liner NOTE For example: the liner can be metallic or not. the liner ensu
42、res the leak tightness of the vessel. 3.2.8 composite over-wrapped pressurized structure (COPS) pressurized structure with a fibre-based composite system fully or partially encapsulating a liner NOTE For example: the liner can be metallic or not. the liner ensures the leak tightness of the vessel. 3
43、.2.9 composite over-wrapped special pressurized equipment (COSPE) special pressurized equipment with a fibre-based composite system fully or partially encapsulating a liner NOTE For example: the liner can be metallic or not. the liner ensures the leak tightness of the vessel. 3.2.10 composite pressu
44、re vessel (CPV) pressure vessel whose structural wall is fully composed with fibre based composite material NOTE For example: the permeation barrier can be ensured by a coating on the internal or the external shape of the composite wall, or by the composite wall itself, or by both. low-pressure liqu
45、id hydrogen tank without liner. 3.2.11 composite pressurized structure (CPS) pressurized structure whose structural wall is fully composed with fibre based composite material BS EN 16603-32-02:2014EN 16603-32-02:2014 (E) 10 NOTE For example: the permeation barrier can be ensured by a coating on the
46、internal or external shape of the composite wall, or by the composite wall itself, or by both. low-pressure liquid hydrogen structural tank without liner. 3.2.12 critical flaw specific flaw with a size such that unstable growth occurs under the specific operating load and environment 3.2.13 cryostat
47、 vacuum-jacketed container designed to keep its contents at a low (cryogenic) temperature NOTE Cryostat is also known as a Dewar, named after its inventor. 3.2.14 design burst pressure differential pressure to be withstood by the pressurized hardware without burst in the applicable operating environ
48、ment NOTE The design burst pressure is equal to the product of the MDP and the burst factor. 3.2.15 differential pressure internal pressure minus external pressure 3.2.16 external pressure absolute pressure outside the pressurized hardware 3.2.17 fibre failure rupture or kinking of a bundle of filam
49、ents NOTE There are two fibre failure modes: under tension (fibre rupture) and under compression (kinking). 3.2.18 fitting pressure component of a pressurized system utilized to connect lines, other pressure components or pressure vessels within the system 3.2.19 hazardous fluid container pressurized container, compartment or housing that is individually sealed to contain a fluid, which can create a hazard if released BS EN 16603-32-02:2014EN 16603-32-02:2014 (E) 11 3.2.20 hydrogen embrittlement mechanical and environmental process that res
