1、BS EN 16602-20-08:2016Space product assurance Storage, handling andtransportation of spacecrafthardwareBSI Standards PublicationWB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06BS EN 16602-20-08:2016 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN16602-20
2、-08:2016.The 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 con
3、tract. Users are responsible for its correctapplication. The British Standards Institution 2016. Published by BSI StandardsLimited 2016ISBN 978 0 580 93135 2ICS 49.140Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authori
4、ty of theStandards Policy and Strategy Committee on 31 August 2016.Amendments issued since publicationDate Text affectedBS EN 16602-20-08:2016EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 16602-20-08 August 2016 ICS 49.140 English version Space product assurance - Storage, handling and transp
5、ortation of spacecraft hardware Assurance produit des projets spatiaux - Stockage, manipulation et transport du matriel dun vhicule spatial Raumfahrtproduktsicherung - Lagerung, Handhabung und Transport von Raumfahrzeug-Hardware This European Standard was approved by CEN on 22 May 2016. CEN and CENE
6、LEC members are bound to comply with the CEN/CENELEC Internal 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 a
7、pplication to the CEN-CENELEC Management Centre or to any 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 not
8、ified to the CEN-CENELEC Management Centre has the same 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 Repub
9、lic 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 United Kingdom. CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brusse
10、ls 2016 CEN/CENELEC All rights of exploitation in any form and by any means reserved worldwide for CEN national Members and for CENELEC Members. Ref. No. EN 16602-20-08:2016 EBS EN 16602-20-08:2016EN 16602-20-08:2016 (E) 2 Table of contents European Foreword . 5 Introduction 6 1 Scope . 7 2 Normativ
11、e references . 8 3 Terms, definitions and abbreviated terms 9 3.1 Terms from other standards 9 3.2 Terms specific to the present standard . 9 3.3 Abbreviated terms. 10 3.4 Nomenclature . 10 3.4.1 Formal verbs . 10 4 General requirements for storage, handling and transportation . 12 4.1 Project phasi
12、ng . 12 4.2 Design considerations 12 4.3 Nonconformance management . 13 4.4 Safety . 13 4.5 Environmental conditions 13 4.6 Packaging and protection material 13 4.7 Certified equipment . 14 4.8 Training 14 5 Storage 15 5.1 General . 15 5.2 Storage implementation 15 5.3 Document requirements 15 5.4 C
13、onfiguration 16 5.4.1 Storage technical configuration . 16 5.4.2 Duration 17 5.4.3 Environmental conditions 17 5.5 Storage activities 17 5.5.1 Pre-storage review (PSR) . 17 BS EN 16602-20-08:2016EN 16602-20-08:2016 (E) 3 5.5.2 Storage area . 17 5.5.3 Traceability . 18 5.5.4 Packing and unpacking act
14、ivities . 18 5.5.5 Periodic inspection and testing 18 5.5.6 Refurbishment and maintenance . 18 5.5.7 Associated hardware . 19 5.5.8 Software 19 5.5.9 Post storage activities . 19 5.6 Retesting after re-assembly 19 5.7 Product knowledge conservation 19 6 Handling 20 6.1 Background 20 6.2 Handling MGS
15、E requirements 20 6.2.1 Easy visual inspection . 20 6.2.2 Hazardous or unsafe configuration 20 6.2.3 MGSE reuse . 20 6.2.4 MGSE loose items 21 6.2.5 Ready for use criteria 21 6.2.6 MGSE logbook 21 6.2.7 MGSE maintenance plan 21 6.2.8 MGSE validation . 22 6.3 Operational requirements . 22 6.3.1 Dedic
16、ated procedure . 22 6.3.2 Operation prerequisite . 22 6.3.3 Attachment points inspection 23 6.3.4 Non-interruptible sequence operation . 23 6.4 Quality requirements . 23 6.4.1 QA witnesses 23 7 Transportation 24 7.1 Categories of transported goods . 24 7.1.1 General . 24 7.1.2 P1 products . 24 7.1.3
17、 P2 products . 24 7.1.4 P3 products . 25 7.2 Categorization of transports 25 7.2.1 Overview . 25 7.2.2 Category of transports to be used . 25 BS EN 16602-20-08:2016EN 16602-20-08:2016 (E) 4 7.3 Transport general requirements 26 7.4 FMEA and risk analysis 27 7.5 Consent to transport (CTT) . 27 7.6 Es
18、cort role and responsibilities . 28 7.6.1 Escort scope and applicability . 28 7.6.2 Duty of the escort 28 7.7 Loading . 29 7.7.1 Background . 29 7.7.2 Requirements 29 7.8 Packaging requirements . 30 7.8.1 General packaging requirements 30 7.8.2 Markings requirements 31 7.9 Transport requirements sum
19、mary . 32 Annex A (normative) Storage plan (SP) DRD 33 A.1 DRD identification . 33 A.1.1 Requirement identification and source document 33 A.1.2 Purpose and objective . 33 A.2 Expected response . 33 A.2.1 Scope and content 33 A.2.2 Special remarks 35 Annex B (informative) Example of a “Movement Plan
20、” 36 Annex C (informative) Example of a “Consent to transport“ . 38 Annex D (informative) Example of a “Packing, shipping, transportation and delivery checklist“ . 48 Annex E (informative) Deliverable per Review List 50 Bibliography . 51 Figures Figure B-1 : Example of Movement Plan 37 Figure D-1 :
21、Packing, shipping, transportation and delivery checklist 49 Tables Table 7-1: Summary of transport requirements 32 Table E-1 : Storage Plan with respected to milestones . 50 BS EN 16602-20-08:2016EN 16602-20-08:2016 (E) 5 European Foreword This document (EN 16602-20-08:2016) has been prepared by Tec
22、hnical Committee CEN-CENELEC/TC 5 “Space”, the secretariat of which is held by DIN. This standard (EN 16602-20-08:2016) originates from ECSS-Q-ST-20-08C. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the late
23、st 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 be held responsible for identifying any or all
24、 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 any EN covering the same scope but with a wider
25、 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, Forme
26、r 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 16602-20-08:2016EN 16602-20-08:2016
27、(E) 6 Introduction This standard focuses on requirements for preservation of space segments and associated hardware. BS EN 16602-20-08:2016EN 16602-20-08:2016 (E) 7 1 Scope The standard specifies requirements to ensure safe handling, storage, transportation of space segment hardware, including assoc
28、iated items to avoid degradation from integration up to launch. The standard is applicable to: Space systems, Space segments, Assembled Spacecraft, Space segment elements, Spacecraft Modules, space segment subsystems, space segment equipment, partly manufactured space segment equipment. Intended pro
29、grams are all space programs and target users all space hardware suppliers and customers. The standard does not cover obsolescence management issues. This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00. NOTE This standard i
30、s applicable to GSE, when mentioned in the different clauses of this standard. BS EN 16602-20-08:2016EN 16602-20-08:2016 (E) 8 2 Normative references The following normative documents contain provisions which, through reference in this text, constitute provisions of this ECSS Standard. For dated ref
31、erences, subsequent amendments to, or revision 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 more recent editions of the normative documents indicated below. For undated references,
32、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 16603-10 ECSS-E-ST-10 Space engineering - System engineering general requirements EN 16603-10-03 ECSS-E-ST-10-03 Space engineering - Testi
33、ng EN 16601-40 ECSS-M-ST-40 Space project management- Configuration and information management EN 16601-80 ECSS-M-ST-80 Space project management - Risk management EN 16602-10 ECSS-Q-ST-10 Space product assurance - Product assurance management EN 16602-10-04 ECSS-Q-ST-10-04 Space product assurance -
34、Critical item control EN 16602-10-09 ECSS-Q-ST-10-09 Space product assurance - Nonconformance control system EN 16602-20 ECSS-Q-ST-20 Space product assurance - Quality assurance EN 16602-30-02 ECSS-Q-ST-30-02 Space product assurance - Failure modes effects (and criticality) analysis EN 16602-40 ECSS
35、-Q-ST-40 Space product assurance - Safety BS EN 16602-20-08:2016EN 16602-20-08:2016 (E) 9 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 particular for the following terms: 1. cle
36、anliness 2. contamination 3. space segment 4. space segment subsystem 5. space segment element 6. cleanliness 7. safety 3.2 Terms specific to the present standard 3.2.1 handling movement, lifting, tilting, rotation, on-site transports, of space hardware NOTE On-site transport is a transport between
37、buildings, without any use of public infrastructures. 3.2.2 storage non-operating phase between two phases of manufacturing, assembly and testing or launch campaign of a space hardware lifetime agreed between a customer and a supplier 3.2.3 transport movement of hardware between two places, using pu
38、blic infrastructure BS EN 16602-20-08:2016EN 16602-20-08:2016 (E) 10 3.3 Abbreviated terms For the purpose of this standard, the abbreviated terms from ECSS-S-ST-00-01 and the following apply: Abbreviation Meaning ABCL as built configuration list AIT assembly, integration and test AR acceptance revi
39、ew BOM bill of materials CIL critical items list CTT consent to transport DRB delivery review board DRD document requirements definition EIDP end item data package ESD electrostatic discharge FMEA failures modes and effect analysis HW hardware ITT invitation to tender MGSE mechanical ground support
40、equipment N/A not applicable NCR nonconformance report PSR pre-storage review QA quality assurance RFD request for deviation RFW request for waiver TOL transport operations leader TRR test readiness review 3.4 Nomenclature 3.4.1 Formal verbs The following nomenclature apply throughout this document:
41、 The word “shall” is used in this document to express requirements. All the requirements are expressed with the word “shall”. The word “should” is used in this document to express recommendations. All the recommendations are expressed with the word “should”. BS EN 16602-20-08:2016EN 16602-20-08:2016
42、 (E) 11 NOTE It is expected that, during tailoring, all the recommendations in this standard are either converted into requirements or tailored out. The words “may” and “need not” are used in this document to express positive and negative permissions respectively. All the positive permissions are ex
43、pressed with the word “may”. All the negative permissions are expressed with the words “need not”. The word “can” is used in this document to express capabilities or possibilities, and therefore, if not accompanied by one of the previous words, it implies descriptive text. NOTE In ECSS “may” and “ca
44、n” have a complete different meaning: “may” is normative (permission) and “can” is descriptive. The present and past tense are used in this document to express statement of fact, and therefore they imply descriptive text. BS EN 16602-20-08:2016EN 16602-20-08:2016 (E) 12 4 General requirements for st
45、orage, handling and transportation 4.1 Project phasing a. The overall activities for handling, storage and transportation shall be planned as part of the normal engineering activities at each project phase in conformance with requirement 5.4.1.1b from ECSS-E-ST-10, b. Handling, storage and transport
46、ation documentation shall be phased with design documents and issued at various reviews. NOTE Guidelines for deliverables per review list are provided in the Annex E. 4.2 Design considerations a. In line with requirement 5.4.1.1b from ECSS-E-ST-10, the design shall not prevent to meet the handling,
47、storage and transportation constraints, as specified in Design Definition File in conformance with DRD from Annex G of ECSS-E-ST-10. b. The flight hardware shall be designed for an lifetime extending from the equipment Delivery Review Board to satellite end of operation lifetime, including specified
48、 storage at any level from unit to space segment element level. c. The satellite design should provide the capability of performing periodic inspection, maintenance and local testing during AIT and on-ground storage without the need to remove equipment or activate the complete satellite. NOTE Exampl
49、e of this maintenance is exercising of mechanisms to allow lubricant redistribution. d. Coherent with specific storage duration of minimum 6 months, the design shall ensure that there is no need for inspection, testing or maintenance during 6 months. e. The need for maintenance and refurbishment shall be derived from the design. BS EN 16602-20-08:2016EN 16602-20-08:2016 (E) 13 f. The design of the flight object shall provide direct access to connectors, test ports and fixation points for AIT operation, handling or transportation. g. Test or stimulus points shall be acces
