EN 50389:2005
(Main)Space product assurance - Wire-wrapping of high-reliability electrical connections
Space product assurance - Wire-wrapping of high-reliability electrical connections
This standard specifies the methods for preparing and assembling the parts to be joined by wire wrapping, and the selection, calibration, use and certification of the wire wrapping tools. The required wirewrapped connections are illustrated in Figure 1. This type of connection is similar to “Class A preferred” or “modified” connection detailed in MIL STD 1130, and NASA NHB 5300.4(3H). Only tested and qualified wirewrapped connections are covered by this standard, which lists four wire sizes from 24 AWG to 30 AWG, and three terminal post sizes up to 1,78 mm maximum diagonal. The use of thicker wire and larger terminals are not advised. Thicker wire than 24 AWG is generally multistranded and terminated by soldering (see ECSS Q 70 08) or by crimping (see ECSS Q 70 26). Training and certification requirements for operators and inspectors are defined in 9.7 and in EN 13291 1.
Raumfahrt-Produktsicherung - Lötfreie elektrische Drahtverbindungen hoher Zuverlässigkeit
Diese Norm legt Verfahren zur Herstellung und Montage der mit lötfreien Drahtwickelverbindungen (im Folgenden kurz 'Wickelverbindungen') zu verbindenden Teile und enthält Angaben zur Auswahl, Kalibrierung, zum Gebrauch und zur Zertifizierung von Wickelwerkzeugen. Bild 1 zeigt eine den Anforderungen entsprechende Wickelverbindung. Wickelverbindungen entsprechen Verbindungen der "Klasse A (empfohlen)" oder "modifizierten" Verbindungen, wie sie in MIL-STD-1130 und NASA NHB 5300.4(3H) festgelegt sind. Diese Norm gilt nur für geprüfte und qualifizierte Wickelverbindungen und bezieht sich auf vier Drahtstärken (AWG 24 bis AWG 30) und drei Stiftgrößen (mit einem Diagonalmaß von maximal 1,78 mm). Die Verwendung von dickerem Draht und größeren Wickelstiften wird nicht empfohlen. Bei Draht-durchmessern von mehr als AWG 24 wird im Allgemeinen Litze mit Lötverbindungen (siehe ECSS Q 70-08) oder Crimpverbindungen (siehe ECSS-Q-70-26) verwendet. Anforderungen an die Schulung und Zertifizierung von Wickel- und Prüfpersonal sind in 9.7 und in EN 13291 1 festgelegt.
Conformité des produits spaciaux - Connexion par enroulement des connexions électriques de haute fiabilité
Zagotavljanje vesoljskih izdelkov - Visoko zanesljivi električni spoji z žičnim ovijanjem
General Information
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EUROPEAN STANDARD EN 50389
NORME EUROPÉENNE
EUROPÄISCHE NORM September 2005
ICS 49.060
English version
Space product assurance –
Wire-wrapping of high-reliability electrical connections
Conformité des produits spaciaux - Raumfahrt-Produktsicherung –
Connexion par enroulement Lötfreie elektrische Drahtverbindungen
des connexions électriques hoher Zuverlässigkeit
de haute fiabilité
This European Standard was approved by CENELEC on 2005-08-01. CENELEC 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
application to the Central Secretariat or to any CENELEC member.
This European Standard exists in two official versions (English, German). A version in any other language
made by translation under the responsibility of a CENELEC member into its own language and notified to the
Central Secretariat has the same status as the official versions.
CENELEC members are the national electrotechnical committees of Austria, Belgium, Cyprus, Czech
Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia,
Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden,
Switzerland and United Kingdom.
CENELEC
European Committee for Electrotechnical Standardization
Comité Européen de Normalisation Electrotechnique
Europäisches Komitee für Elektrotechnische Normung
Central Secretariat: rue de Stassart 35, B - 1050 Brussels
© 2005 CENELEC - All rights of exploitation in any form and by any means reserved worldwide for CENELEC members.
Ref. No. EN 50389:2005 E
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EN 50389:2005 - 2 -
Foreword
This European Standard was prepared by the Technical Committee CENELEC TC 107X, Process
management for avionics (former CENELEC BTTF 91-3).
The text of the draft was submitted to the formal vote and was approved by CENELEC as EN 50389 on
2005-08-01.
The following dates were fixed:
– latest date by which the EN has to be implemented
at national level by publication of an identical
national standard or by endorsement (dop) 2006-08-01
– latest date by which the national standards conflicting
with the EN have to be withdrawn
(dow) 2008-08-01
1)
It is based on a previous version originally prepared by the ECSS product assurance working group,
reviewed by the ECSS Technical Panel and approved by the ECSS Steering Board. The European
Cooperation for Space Standardization (ECSS) is a cooperative effort of the European Space Agency,
National Space Agencies and European industry associations for the purpose of developing and
maintaining common standards.
This European Standard is one of a series of space standards intended to be applied together for the
management, engineering and product assurance in space projects and applications.
Requirements in this European Standard are defined in terms of what shall be accomplished, rather than
in terms of how to organize and perform the necessary work. This allows existing organizational
structures and methods to be applied where they are effective, and for the structures and methods to
evolve as necessary without rewriting the standards.
The formulation of this European Standard takes into account the existing EN ISO 9000 family of
documents.
———————
1)
ECSS-Q-70-30A.
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- 3 - EN 50389:2005
Contents
Introduction.5
1 Scope.5
2 Normative references .6
3 Terms, definitions and abbreviated terms .7
3.1 Terms and definitions .7
3.2 Abbreviated terms .8
4 Preparatory conditions.
...
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