BS EN 16602-70-71-2016 Space product assurance Materials processes and their data selection《航天产品保证 材料 过程及其数据采集》.pdf

《BS EN 16602-70-71-2016 Space product assurance Materials processes and their data selection《航天产品保证 材料 过程及其数据采集》.pdf》由会员分享，可在线阅读，更多相关《BS EN 16602-70-71-2016 Space product assurance Materials processes and their data selection《航天产品保证 材料 过程及其数据采集》.pdf（42页珍藏版）》请在麦多课文档分享上搜索。

1、BS EN 16602-70-71:2016Space product assurance Materials, processes and theirdata selectionBSI Standards PublicationWB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06BS EN 16602-70-71:2016 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN16602-70-71:2016.The

2、UK participation in its preparation was entrusted 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

3、are responsible for its correctapplication. The British Standards Institution 2016. Published by BSI StandardsLimited 2016ISBN 978 0 580 93134 5ICS 49.140Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStan

4、dards Policy and Strategy Committee on 31 August 2016.Amendments issued since publicationDate Text affectedBS EN 16602-70-71:2016EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 16602-70-71 August 2016 ICS 49.140 English version Space product assurance - Materials, processes and their data selec

5、tion Assurance produit des projets spatiaux - Matriaux, procds et les donnes pour leur slection Raumfahrtproduktsicherung - Werkstoffe, Prozesse und Angaben zu ihrer Auswahl This European Standard was approved by CEN on 22 May 2016. CEN and CENELEC members are bound to comply with the CEN/CENELEC In

6、ternal Regulations which stipulate the 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 a

7、ny CEN and CENELEC member. This European 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

8、 status as the official versions. CEN and 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, Ice

9、land, Ireland, Italy, Latvia, Lithuania, 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 2016 CEN/CENELEC All rights of exploitation in any f

10、orm and by any means reserved worldwide for CEN national Members and for CENELEC Members. Ref. No. EN 16602-70-71:2016 EBS EN 16602-70-71:2016EN 16602-70-71:2016 (E ) 2 Table of contents European Foreword . 4 1 Scope . 5 2 Normative references . 6 3 Terms, definitions and abbreviated terms 8 3.1 Ter

11、ms from other standards 8 3.2 Terms specific to the present standard . 8 3.3 Abbreviated terms. 9 3.4 Nomenclature . 10 4 Specific requirements 11 4.1 Overview 11 4.2 Material requirements . 11 4.2.1 General requirements . 11 4.2.2 Aluminium and aluminium alloys . 11 4.2.3 Copper and copper alloys .

12、 12 4.2.4 Nickel and nickel alloys . 12 4.2.5 Titanium and Titanium alloys . 12 4.2.6 Steels 13 4.2.7 Stainless steels . 13 4.2.8 Filler metals: welding, brazing, soldering . 13 4.2.9 Miscellaneous metallic materials . 14 4.2.10 Optical materials . 15 4.2.11 Adhesives, coatings, varnishes . 15 4.2.1

13、2 Adhesive tapes . 16 4.2.13 Paints and inks 17 4.2.14 Lubricants . 17 4.2.15 Potting compounds, sealants, foams . 18 4.2.16 Reinforced plastics including PCBs . 18 4.2.17 Rubbers and elastomers . 19 4.2.18 Thermoplastics 20 BS EN 16602-70-71:2016EN 16602-70-71:2016 (E ) 3 4.2.19 Thermoset plastics

14、or PCBs 21 4.2.20 Material aspects of wires and cables . 21 4.2.21 Ceramics and other nonmetallic materials . 22 4.3 Process requirements . 22 4.3.1 Adhesive bonding . 22 4.3.2 Composite manufacture 23 4.3.3 Encapsulation and moulding and varnishing . 23 4.3.4 Painting and coating 24 4.3.5 Cleaning

15、24 4.3.6 Welding and brazing . 24 4.3.7 Crimping and stripping and wire wrapping . 26 4.3.8 Soldering . 26 4.3.9 Surface treatments 26 4.3.10 Plating . 28 4.3.11 Machining . 29 4.3.12 Forming . 30 4.3.13 Heat treatment 32 4.3.14 Marking . 32 4.3.15 Miscellaneous processes 32 4.3.16 Inspection proced

16、ures . 34 Annex A (informative) Information about the European Space Materials Database (ESMDB) 35 A.1 Overview 35 A.2 Database access 35 A.3 Database structure . 35 A.4 Database quality ratings . 37 Bibliography . 38 BS EN 16602-70-71:2016EN 16602-70-71:2016 (E ) 4 European Foreword This document (

17、EN 16602-70-71:2016) has been prepared by Technical Committee CEN-CENELEC/TC 5 “Space”, the secretariat of which is held by DIN. This standard (EN 16602-70-71:2016) originates from ECSS-Q-ST-70-71C. This European Standard shall be given the status of a national standard, either by publication of an

18、identical text or by endorsement, at the latest by February 2017, and conflicting national standards shall be withdrawn at the latest by February 2017. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC shall not b

19、e held responsible for identifying any or all such patent rights. This document has been prepared under a mandate given to CEN by the European Commission and the European Free Trade Association. This document has been developed to cover specifically space systems and has therefore precedence over an

20、y EN covering the same scope but with a wider 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, Cze

21、ch Republic, Denmark, Estonia, Finland, Former 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 Kingdo

22、m. BS EN 16602-70-71:2016EN 16602-70-71:2016 (E ) 5 1 Scope This Standard specifies the requirements applicable to materials, processes and their data selection to satisfy the mission performance requirements. This Standard covers the following: selection criteria and rules; utilization criteria and

23、 rules. The provisions of this Standard apply to all actors involved at all levels in the production of space systems. These can include manned and unmanned spacecraft, launchers, satellites, payloads, experiments, electrical ground support equipment, mechanical ground support equipment, and their c

24、orresponding organizations. This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00. BS EN 16602-70-71:2016EN 16602-70-71:2016 (E ) 6 2 Normative references The following normative documents contain provisions which, through

25、reference in this text, constitute provisions of this ECSS Standard. For dated references, subsequent amendments to, or revisions of any of these publications do not apply. However, parties to agreements based on this ECSS Standard are encouraged to investigate the possibility of applying the most r

26、ecent 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 ECSS system - Glossary of terms EN 16603-20-06 ECSS-E-ST-20-06 Space engineering - Spacecra

27、ft charging EN 16603-32-08 ECSS-E-ST-32-08 Space engineering - Materials 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 EN 16602-70-02 ECSS-Q-ST-70-02 Space product assurance - Thermal

28、vacuum outgassing test for the screening of space materials EN 16602-70-04 ECSS-Q-ST-70-04 Space product assurance - Thermal testing for the evaluation of space materials, processes, mechanical parts and assemblies EN 16602-70-07 ECSS-Q-ST-70-07 Space product assurance - Verification and approval of

29、 automatic machine wave soldering EN 16602-70-08 ECSS-Q-ST-70-08 Space product assurance - Manual soldering of high-reliability electrical connections EN 16602-70-10 ECSS-Q-ST-70-10 Space product assurance - Qualification of printed circuit boards EN 16602-70-11 ECSS-Q-ST-70-11 Space product assuran

30、ce - Procurement of printed circuit boards EN 16602-70-12 ECSS-Q-ST-70-12 Space product assurance - Design rules for printed circuit boards EN 16602-70-18 ECSS-Q-ST-70-18 Space product assurance - Preparation, assembly and mounting of RF coaxial cables EN 16602-70-26 ECSS-Q-ST-70-26 Space product as

31、surance - Crimping of high-reliability electrical connections BS EN 16602-70-71:2016EN 16602-70-71:2016 (E ) 7 EN 16602-70-28 ECSS-Q-ST-70-28 Space product assurance - Repair and modification of printed circuits board assemblies for space use EN 16602-70-30 ECSS-Q-ST-70-30 Space product assurance -

32、Wire wrapping of high-reliability electrical connections EN 16602-70-31 ECSS-Q-ST-70-31 Space product assurance - Application of paints on flight hardware EN 16602-70-38 ECSS-Q-ST-70-38 Space product assurance - High-reliability soldering for surface-mount and mixed technology EN 16602-70-39 ECSS-Q-

33、ST-70-39 Space product assurance - Processing and quality assurance requirements for welding of metallic materials for flight hardware ESCC 3901 Generic specification - Wires and cables, electrical, 600V, low frequency ESCC 3902 Generic specification - Cables, coaxial, radio frequency, flexible ESCC

34、 3903 Generic specification - Solid wires, electrical 350 V, for wire wrapping BS EN 16602-70-71:2016EN 16602-70-71:2016 (E ) 8 3 Terms, definitions and abbreviated terms 3.1 Terms from other standards a. For the purpose of this Standard, the terms and definitions from ECSS-S-ST-00-01 apply, in part

35、icular for the following terms: 1. assembly 2. component 3. corrosion 4. lot 5. material 6. part 7. process 8. relifing 9. repair b. For the purpose of this Standard, the terms and definitions from ECSS-E-ST-32 apply, in particular for the following terms: 1. A-basis design allowable (A-value) 2. B-

36、basis design allowable (B-value) 3.2 Terms specific to the present standard 3.2.1. plate form of material having a thickness of 6 mm 3.2.2. sheet form of material having a thickness 0,2 mm and 1225 MPa UTS. b. Tempers of precipitation hardening steels that are susceptible to stress corrosion and hyd

37、rogen embrittlement shall not be used. c. Designs using precipitation hardening steels shall ensure the following: 1. controlled processing procedures are used, and 2. processing and procurement records are maintained for the reference. 4.2.7 Stainless steels a. Unstabilized austenitic steels shall

38、not be used at temperatures above 370 C. b. When using 400-series stainless steels the risk for hydrogen embrittlement, corrosion and stress corrosion cracking shall be controlled. c. Control means shall be presented for customer approval. 4.2.8 Filler metals: welding, brazing, soldering a. The sele

39、ction of alloys to be welded and the selection of process techniques shall be in conformance with national or international aerospace specifications and standards approved by the customer. b. The fusion zone and the unmelted heat affected zone of a weld shall be accessible for inspection. c. All wel

40、ds used for structural applications shall undergo 100 % radiographic inspection in conformance with specifications approved by the customer. d. All welds used for structural applications shall undergo a NDI program that shall be submitted for customer approval. NOTE ECSS-E-ST-32-01 contains addition

41、al requirements specific to welds used for Potential Fracture Critical Items applications. e. The capability of the equipment to meet the specified requirements, processes, welding supplies and supplementary treatments selected by the supplier shall be demonstrated through qualification testing of w

42、elded specimens representing the materials and joint configuration of production parts. f. The selection of brazing alloys and brazing techniques shall be in conformance with national or international aerospace specifications and standards approved by the customer. BS EN 16602-70-71:2016EN 16602-70-

43、71:2016 (E ) 14 g. Design shall include the effect of the brazing process on the strength of the parent metal. NOTE Base metal is the example of the parent metal. h. Subsequent fusion welding in the vicinity of brazed or soldered joints or other operations with high temperatures that affect the braz

44、ed or soldered joint shall not be performed. i. Soldered joints shall not be used for structural applications. j. Solders, process materials and procedures for electrical and electronic assembly shall conform to the requirements from clause 5 to clause 15 of ECSS-Q-ST-70-08 and from clause 5 to clau

45、se 16 of ECSS-Q-ST-70-38. 4.2.9 Miscellaneous metallic materials a. The supplier shall demonstrate that the selected Magnesium alloys are protected against corrosion effects with respect to the applicable environment. b. Hazards related to Magnesium alloys flammability during manufacturing shall be

46、prevented. c. The supplier shall demonstrate that the selected Magnesium alloys are used in applications where risks of ignition are prevented. NOTE Examples of risk areas are those subjected to wear, abuse, foreign object damage, abrasion, erosion or at any location where fluid or moisture entrapme

47、nt is possible. d. Alloys containing Beryllium higher than 4 % by weight shall not be used. e. The design of parts made of beryllium alloys shall include the materials low impact resistance, notch sensitivity, its anisotropy and sensitivity to surface finish requirements. f. The application of refra

48、ctory alloys shall be subjected to approval by the customer. NOTE Limited amount of data for structural assessment are available on these materials. g. Silver and Osmium coatings shall not be used on external surfaces of space systems exposed to atomic oxygen in low Earth orbit. h. Platings with ope

49、n porosity shall be sealed. i. The selection of a superalloy for a given application shall be based on tests of the material in simulated in-service environments. j. Foreign material which contains sulphur shall be removed from superalloys prior to heat treatment or high-temperature service. NOTE Examples of materials that can contain sulphur are: oils, grease and cutting lubricants. k. The effect of alloying element depletion in superalloys at the surface in a high-temperature oxidizing environment shall be evaluated when sheet is used. BS EN 16602-70-71:2016EN 16602-70-