BS ISO 15859-3-2004 Aerospace series - Space systems - Fluid characteristics sampling and test methods - Nitrogen《航空航天系列 航天系统 流体特性、抽样和试验方法 氮》.pdf
《BS ISO 15859-3-2004 Aerospace series - Space systems - Fluid characteristics sampling and test methods - Nitrogen《航空航天系列 航天系统 流体特性、抽样和试验方法 氮》.pdf》由会员分享,可在线阅读,更多相关《BS ISO 15859-3-2004 Aerospace series - Space systems - Fluid characteristics sampling and test methods - Nitrogen《航空航天系列 航天系统 流体特性、抽样和试验方法 氮》.pdf(18页珍藏版)》请在麦多课文档分享上搜索。
1、BRITISH STANDARD AEROSPACE SERIES BS ISO 15859-3:2004 Space systems Fluid characteristics, sampling and test methods Part 3: Nitrogen ICS 49.140 BS ISO 15859-3:2004 This British Standard was published under the authority of the Standards Policy and Strategy Committee on 16 August 2004 BSI 16 August
2、2004 ISBN 0 580 44267 5 National foreword This British Standard reproduces verbatim ISO 15859-3:2004 and implements it as the UK national standard. The UK participation in its preparation was entrusted by Technical Committee ACE/68, Space systems and operations, to Subcommittee ACE/68/-/3, Operation
3、s and ground support, which has the responsibility to: A list of organizations represented on this subcommittee can be obtained on request to its secretary. Cross-references The British Standards which implement international publications referred to in this document may be found in the BSI Catalogu
4、e under the section entitled “International Standards Correspondence Index”, or by using the “Search” facility of the BSI Electronic Catalogue or of British Standards Online. This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correc
5、t application. Compliance with a British Standard does not of itself confer immunity from legal obligations. aid enquirers to understand the text; present to the responsible international/European committee any enquiries on the interpretation, or proposals for change, and keep the UK interests infor
6、med; monitor related international and European developments and promulgate them in the UK. Summary of pages This document comprises a front cover, an inside front cover, the ISO title page, pages ii to iv, pages 1 to 10, an inside back cover and a back cover. The BSI copyright notice displayed in t
7、his document indicates when the document was last issued. Amendments issued since publication Amd. No. Date Comments Reference number ISO 15859-3:2004(E)INTERNATIONAL STANDARD ISO 15859-3 First edition 2004-06-01 Space systems Fluid characteristics, sampling and test methods Part 3: Nitrogen Systmes
8、 spatiaux Caractristiques, chantillonnage et mthodes dessai des fluides Partie 3: Azote BSISO158593:2004ii BSISO158593:2004ISO 15859-3:2004(E) iiiForeword ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of
9、preparing International Standards is normally carried out through ISO technical committees. Each member body interested in a subject for which a technical committee has been established has the right to be represented on that committee. International organizations, governmental and non-governmental,
10、 in liaison with ISO, also take part in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization. International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 2. The main t
11、ask of technical committees is to prepare International Standards. Draft International Standards adopted by the technical committees are circulated to the member bodies for voting. Publication as an International Standard requires approval by at least 75 % of the member bodies casting a vote. Attent
12、ion is drawn to the possibility that some of the elements of this document may be the subject of patent rights. ISO shall not be held responsible for identifying any or all such patent rights. ISO 15859-3 was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 14,
13、 Space systems and operations. ISO 15859 consists of the following parts, under the general title Space systems Fluid characteristics, sampling and test methods: Part 1: Oxygen Part 2: Hydrogen Part 3: Nitrogen Part 4: Helium Part 5: Nitrogen tetroxide propellants Part 6: Monomethylhydrazine propell
14、ant Part 7: Hydrazine propellant Part 8: Kerosine propellant Part 9: Argon Part 10: Water Part 11: Ammonia Part 12: Carbon dioxide Part 13: Breathing air BSISO158593:2004ISO 15859-3:2004(E) iv Introduction Fluid operations at a spaceport or launch site may involve a number of operators and supplier/
15、customer interfaces, from the fluid production plant to the delivery to the launch vehicle or spacecraft. The purpose of ISO 15859 is to establish uniform requirements for the components, sampling and test methods of fluids used in the servicing of launch vehicles, spacecraft and ground support equi
16、pment. The fluid composition limits specified are intended to define the purity and impurity limits of the fluid for loading into the launch vehicle or spacecraft. The fluid sampling and test methods are intended to be applied by any operator. The fluid sampling and test methods are acceptable metho
17、ds for verification of the fluid composition limits. BSISO158593:2004INTENRATIONAL TSANDADR IS-95851 O3:(4002E)1Space systems Fluid characteristics, sampling and test methods Part 3: Nitrogen 1 Scope This part of ISO 15859 specifies limits for the composition of nitrogen and establishes the sampling
18、 and test requirements applicable for the verification of nitrogen composition. This part of ISO 15859 is applicable to nitrogen, used in both flight hardware and ground facilities, systems and equipment, of the following types and grades of nitrogen. Type I: gaseous Grade A: purging/pressurizing, G
19、rade B: crew breathing, Grade C, Grade F, Grade J; Type II: liquid Grade A: purging/pressurizing, Grade B: crew breathing, Grade C, Grade F. This part of ISO 15859 is applicable to influents only within the specified limits herein. This part of ISO 15859 is applicable to any sampling operation requi
20、red to ensure that, when the fluid enters the launch vehicle or spacecraft, the fluid composition complies with the limits provided hereafter or with any technical specification agreed to for a particular use. 2 Normative references The following referenced documents are indispensable for the applic
21、ation 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. ISO 9000, Quality management systems Fundamentals and vocabulary BSISO158593:2004ISO 15859-3:2004(E) 2 3 Terms and d
22、efinitions For the purposes of this document, the terms and definitions given in ISO 9000 and the following apply. 3.1 direct method method of measuring fluid purity by direct means as opposed to the indirect method NOTE A measurement device or analyser can be used as a direct means for measuring th
23、e fluid purity. 3.2 indirect method method of measuring fluid purity by indirect means, which consists in measuring the total volume fraction or mass fraction (in %) of aggregate impurities and subtracting this total from 100 % 3.3 total hydrocarbon content (as methane) single carbon atom equivalent
24、 3.4 verification test analysis performed on the fluid in the container, or a sample thereof, which is representative of the supply, permitting the verification of fluid composition limits 4 Chemical composition Unless otherwise provided in an applicable technical specification, the composition of n
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