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BS EN 16602-70-26:2019 – TC:2020 Edition

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Tracked Changes. Space product assurance. Crimping of high-reliability electrical connections

Published By Publication Date Number of Pages
BSI 2020 126
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This Standard specifies: • Requirements for the following crimping wire terminations intended for high reliability electrical connections for use on customer spacecraft and associated equipment operating under high vacuum, thermal cycling and launch vibration: • removable contacts, single wires • removable contacts, multiple wires • coaxial connectors, ferrules • lugs and splices. NOTE These are the most common used crimping wire termination and are represented in Figure 1 1. • The general conditions to be met for the approval of terminations other than the above mentioned ones. NOTE Additional forms of crimps, not covered in this standard, are listed (not exhaustively) in the informative Annex A. • Product assurance provisions for both the specific and the generic terminations mentioned above. • Training and certification requirements for operators and inspectors (clause 5.5.2), additional to those specified in ECSS Q ST-20. This standard may be tailored for the specific characteristics and constraints of a space project, in conformance with ECSS-S-ST-00.

PDF Catalog

PDF Pages PDF Title
70 undefined
77 1 Scope
79 2 Normative references
81 3 Terms, definitions and abbreviated terms
3.1 Terms defined in other standards
3.2 Terms specific to the present standard
82 3.3 Abbreviated terms
83 3.4 Nomenclature
84 4 Principles
85 5 Requirements
5.1 Preparatory conditions
5.1.1 Facilities
5.1.1.1 Overview
5.1.1.2 Facility cleanliness
5.1.1.3 Environmental conditions
86 5.1.1.4 Lighting requirements
5.1.2 Tools and equipment
5.1.2.1 Crimping tools
87 5.1.2.2 Insulation strippers
88 5.1.2.3 Cutting pliers
5.1.2.4 Test and monitoring equipment
5.2 Crimping operations for different types of interconnections
5.2.1 General
89 5.2.2 Material selection
90 5.2.3 Process review and documentation
5.2.4 Contact barrel and single wire crimping
91 5.2.5 Contact barrel and multiple wire crimping
93 5.2.6 Ferrule shield crimping
5.2.7 Lug and splice wire crimping
96 5.3 Requirements for crimp configuration qualification
5.3.1 General
97 5.3.2 Qualification process test procedure
99 5.3.3 Sealing and marking
5.3.4 Batch to batch variation
5.3.4.1 Wires qualified by ESCC
5.3.4.2 Wires not qualified by ESCC
5.4 Test methods
5.4.1 General
5.4.2 <>
100 5.4.3 Tensile strength
5.4.3.1 General
5.4.3.2 Contact barrel wire crimping
5.4.3.3 Ferrule
5.4.3.4 Lug and splice
101 5.4.3.5 Characterisation of intrinsic wire / braid strength
5.4.4 Metallography
102 5.5 Quality assurance
5.5.1 General
5.5.2 Personnel training and certification
5.5.2.1 Training program
5.5.2.2 Certification
103 5.5.2.3 Documentation
105 5.5.3 Workmanship
107 5.5.4 Visual inspection
5.5.4.1 Pre-crimp inspection (performed by the operator)
108 5.5.4.2 Post-crimp inspection (performed by quality assurance)
5.5.4.3 General
109 5.5.5 Shift performance inspection and test for harness manufacturing
110 5.5.6 Calibration of crimping tools
5.5.6.1 General
111 5.5.6.2 Validation
5.5.6.3 Sealing and marking
5.5.6.4 Out-of-calibration tools
5.5.7 Records
112 5.5.8 Nonconformance
5.5.9 Special crimping activities at spacecraft level, modifications and repairs
115 5.6 Document requirements
BS EN 16602-70-26:2019 - TC
$258.95