INTERNATIONAL STANDARD ISO 14951-6 First edition 1999-10-01 Dit document mag slechts op een stand-alone PC worden geinstalleerd. Gebruik op een netwerk is alleen. toestaan als een aanvullende licentieovereenkomst voor netwerkgebruik met NEN is afgesloten. This document may only be used on a stand-alone PC. Use in a network is only permitted when a supplementary license agreement for us in a network with NEN has been concluded. Space systems Fluid characteristics Part 6: Monomethylhydrazine propellant Systèmes spatiaux Caractéristiques des fluides Partie 6: Monométhylhydrazine carburant A Reference number ISO 14951-6:1999(E)
ISO 14951-6:1999(E) Foreword ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of 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, 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 3. 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. International Standard ISO 14951-6 was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 14, Space systems and operations. ISO 14951 consists of the following parts, under the general title Space systems Fluid characteristics: Part 1: Oxygen Part 2: Hydrogen propellant Part 3: Nitrogen Part 4: Helium Part 5: Nitrogen tetroxide propellant Part 6: Monomethylhydrazine propellant Part 7: Hydrazine propellant Part 8: Kerosene propellant Part 9: Argon Part 10: Water Part 11: Ammonia Part 12: Carbon dioxide Part 13: Breathing air ISO 1999 All rights reserved. Unless otherwise specified, no part of this publication may be reproduced or utilized in any form or by any means, electronic or mechanical, including photocopying and microfilm, without permission in writing from the publisher. International Organization for Standardization Case postale 56 CH-1211 Genève 20 Switzerland Internet iso@iso.ch Printed in Switzerland ii
INTERNATIONAL STANDARD ISO ISO 14951-6:1999(E) Space systems Fluid characteristics Part 6: Monomethylhydrazine propellant 1 Scope This part of ISO 14951 specifies limits for the composition of monomethylhydrazine (N 2 H 3 CH 3 ) (MMH) propellant and test methods for verification of propellant composition. This part of ISO 14951 is applicable to monomethylhydrazine propellant of the following grades, intended for use as a fuel in propellant systems of space systems: grade A: 98,0 % pure; grade F: 98,5 % pure. This part of ISO 14951 is applicable to propellant used in both flight hardware and ground facilities, systems, and equipment. It is applicable to influents only to the extent specified herein. CAUTION Monomethylhydrazine, in the liquid or vapour form, is toxic and volatile. Care should be taken in the handling and storage of monomethylhydrazine to prevent contact with the human body and with materials that are not compatible. 2 Term and definition For the purposes of this part of ISO 14951, the following term and definition apply. 2.1 particulate undissolved solids retained on a filter paper with a 10 µm nominal and 40 µm absolute rating 3 Composition The composition of MMH propellant delivered to the flight vehicle interface shall be in accordance with the limits given in Table 1 when tested in accordance with the applicable test methods. 4 Qualitative properties The propellant shall be a homogeneous liquid when examined visually by transmitted light. 1
ISO 14951-6:1999(E) ISO 5 Test methods 5.1 Sampling The propellant should be selected in accordance with a sampling plan that will produce results with sensitivities and accuracies equivalent to or better than those required to meet the programme or project requirements. 5.2 Composition tests The composition of the propellant shall be tested by such methods, apparatus, or analyzers as may be required to produce results with the sensitivities and accuracies necessary to meet programme or project requirements. Table 1 Composition limits Composition Grade A Limits Grade F Monomethylhydrazine assay mass fraction, %, min. 98,0 98,5 Water mass fraction, %, max. 2,0 0,5 Particulate mg/l, max. 10 10 Natrium µg/g, max. 2 NH 3 mass fraction, %, max. 0,2 Monomethylamine mass fraction, %, max. 0,3 2
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