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BS EN 16603-20-07:2022 – TC:2023 Edition

$280.87

Tracked Changes. Space engineering. Electromagnetic compatibility

Published By Publication Date Number of Pages
BSI 2023 218
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PDF Catalog

PDF Pages PDF Title
1 30467226
113 A-30437740
114 undefined
124 1 Scope
125 2 Normative references
126 3 Terms, definitions and abbreviated terms
3.1 Terms from other standards
127 3.2 Terms specific to the present standard
129 3.3 Abbreviated terms
131 4 Requirements
4.1 General system requirements
4.2 Detailed system requirements
4.2.1 Overview
4.2.2 EMC with the launch system
4.2.2.1 Overview
4.2.2.2 Detailed system requirements
132 4.2.3 Lightning environment
4.2.3.1 Overview
4.2.3.2 Requirements to the space system
4.2.4 Spacecraft charging and effects
4.2.4.1 Overview
4.2.4.2 EMI control requirements to system and equipment in relation with ESD
133 4.2.5 Spacecraft DC magnetic emission
4.2.5.1 Spacecraft with susceptible payload
4.2.5.2 Attitude control system (ACS)
4.2.6 Radiofrequency compatibility
134 4.2.7 Hazards of electromagnetic radiation
4.2.8 Intrasystem EMC
4.2.9 EMC with ground equipment
135 4.2.10 Grounding
4.2.10.1 Overview
4.2.10.2 Requirements
4.2.11 Electrical bonding requirements
4.2.11.1 Overview
136 4.2.11.2 Normative provisions
4.2.11.3 External grounds
137 4.2.12 Shielding (except wires and cables)
4.2.12.1 Overview
4.2.12.2 Requirements
4.2.13 Wiring (including wires and cables shielding)
4.2.13.1 Classification of cables
4.2.13.2 Cable shields
139 5 Verification
5.1 Overview
5.1.1 Introduction
5.1.2 Electromagnetic effects verification plan
5.1.3 Electromagnetic effects verification report
5.2 Test conditions
5.2.1 Measurement tolerances
140 5.2.2 Test site
5.2.2.1 Overview
5.2.2.2 Shielded enclosures
141 5.2.2.3 Ambient electromagnetic level
5.2.2.4 Ambient conducted level
142 5.2.3 Ground plane
5.2.3.1 General
5.2.3.2 Metallic ground plane
5.2.3.3 Composite ground plane
5.2.4 Power source impedance
144 5.2.5 General test precautions
5.2.5.1 Safety
5.2.5.2 Excess personnel and equipment
5.2.5.3 Overload precautions
5.2.6 EUT test configurations
5.2.6.1 General
145 5.2.6.2 Bonding of EUT
5.2.6.3 Shock and vibration isolators
5.2.6.4 Safety grounds
5.2.6.5 Orientation of EUTs
146 5.2.6.6 Construction and arrangement of EUT cables
147 5.2.6.7 Electrical and mechanical interfaces
5.2.7 Operation of EUT
5.2.7.1 General
148 5.2.7.2 Operating frequencies for tuneable RF equipment
5.2.7.3 Operating frequencies for spread spectrum equipment
5.2.7.4 Susceptibility monitoring
5.2.8 Use of measurement equipment
5.2.8.1 Overview
149 5.2.8.2 Detector
5.2.8.3 Calibration fixture (jig)
150 5.2.9 Emission testing
5.2.9.1 Bandwidths
5.2.9.2 Emission identification
5.2.9.3 Frequency scanning
151 5.2.9.4 Emission data presentation
5.2.10 Susceptibility testing
5.2.10.1 Frequency stepping
152 5.2.10.2 Modulation of susceptibility signals
153 5.2.10.3 Thresholds of susceptibility
5.2.10.4 Susceptibility data presentation
5.2.11 Calibration of measuring equipment
5.2.11.1 General
5.2.11.2 Measurement system test
154 5.2.12 Power bus voltage
5.2.13 Photographic data
5.3 System level
5.3.1 General
5.3.2 Safety margin demonstration for critical or EED circuits
155 5.3.3 EMC with the launch system
5.3.4 Lightning
5.3.5 Spacecraft and static charging
156 5.3.6 Spacecraft DC magnetic field emission
5.3.7 Intra–system electromagnetic compatibility
5.3.8 Radiofrequency compatibility
5.3.9 Grounding
5.3.10 Electrical bonding
5.3.11 Wiring and shielding
157 5.4 Equipment and subsystem level test procedures
5.4.1 Overview
5.4.2 CE, power leads, differential mode, 30 Hz to 100 kHz
5.4.2.1 Purpose
5.4.2.2 Test equipment
158 5.4.2.3 Setup
5.4.2.4 Procedure
159 5.4.3 CE, power and signal leads, 50 kHz to 100 MHz
5.4.3.1 Purpose
160 5.4.3.2 Test equipment
5.4.3.3 Setup
161 5.4.3.4 Procedures
162 5.4.4 CE, power leads, inrush current
5.4.4.1 Purpose
5.4.4.2 Test equipment
163 5.4.4.3 Setup
164 5.4.4.4 Procedures
165 5.4.4.5 Data presentation
5.4.5 DC Magnetic field emission, magnetic moment
5.4.5.1 Overview
166 5.4.5.2 Set-Up
5.4.5.3 Test sequence
167 5.4.5.4 Data presentation
168 5.4.6 RE, electric field, 30 MHz to 18 GHz
5.4.6.1 Purpose
5.4.6.2 Test equipment
169 5.4.6.3 Test setup
171 5.4.6.4 Test procedures
172 5.4.6.5 Data Presentation
5.4.7 CS, power leads, 30 Hz to 100 kHz
5.4.7.1 Purpose
5.4.7.2 Test equipment
173 5.4.7.3 Setup
174 5.4.7.4 Procedures
175 5.4.8 CS, bulk cable injection, 50 kHz to 100 MHz
5.4.8.1 Purpose
5.4.8.2 Test equipment
5.4.8.3 Setup
176 5.4.8.4 Test procedures
179 5.4.9 CS, power leads, transients
5.4.9.1 Purpose
5.4.9.2 Test equipment
180 5.4.9.3 Setup
182 5.4.9.4 Procedures
183 5.4.10 RS, magnetic field, 30 Hz to 100 kHz
5.4.10.1 Purpose
5.4.10.2 Test equipment
5.4.10.3 Setup
184 5.4.10.4 Test procedures
185 5.4.10.5 Data Presentation
186 5.4.11 RS, electric field, 30 MHz to 18 GHz
5.4.11.1 Purpose and overview
5.4.11.2 Test equipment
187 5.4.11.3 Test setup
190 5.4.11.4 Test procedures
192 5.4.11.5 Test report content and data presentation
193 5.4.12 Susceptibility to wire-coupled electrostatic discharges (legacy method)
5.4.12.1 Overview
5.4.12.2 Test equipment
194 5.4.12.3 Setup
196 5.4.12.4 Procedure
197 5.4.12.5 Data presentation
198 5.4.13 Susceptibility to wire-coupled electrostatic discharges (current injection probe method)
5.4.13.1 Overview
5.4.13.2 Test equipment
5.4.13.3 Calibration
200 5.4.13.4 EUT testing
201 5.4.13.5 Data presentation
5.4.14 Susceptibility to electrostatic discharges into the chassis
5.4.14.1 Overview
5.4.14.2 Test equipment
202 5.4.14.3 Test setup
5.4.14.4 Procedure
204 5.4.14.5 Data presentation
5.4.15 CE, power leads, time domain
5.4.15.1 Purpose
5.4.15.2 Test equipment
5.4.15.3 Test setup
205 5.4.15.4 Procedure
5.4.15.5 Data presentation
BS EN 16603-20-07:2022 - TC
$280.87