ISO 24637:2009
(Main)Space systems — Electromagnetic interference (EMI) test reporting requirements
Space systems — Electromagnetic interference (EMI) test reporting requirements
ISO 24637:2009 provides specific requirements for the content of equipment-level electromagnetic interference (EMI) test report documentation to ensure that sufficient data is provided for subsequent integration analysis of complex space systems. Emphasis is placed on necessary test report augmentation to include additional test data reporting when specifically needed to document any EMI test limit failures for spaceflight hardware. The requirements presented in ISO 24637:2009 apply only to EMI test reports at the equipment level. These requirements are particularly important when an EMI test limit non-conformance waiver is requested for spaceflight equipment in lieu of re-design.
Systèmes spatiaux — Exigences pour l'enregistrement de l'essai d'interférences électromagnétiques (EMI)
General Information
Standards Content (Sample)
INTERNATIONAL ISO
STANDARD 24637
First edition
2009-02-15
Space systems — Electromagnetic
interference (EMI) test reporting
requirements
Systèmes spatiaux — Exigences pour l'enregistrement de l'essai
d'interférences électromagnétiques (EMI)
Reference number
©
ISO 2009
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ii © ISO 2009 – All rights reserved
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 2.
The main task 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.
Attention 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 24637 was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 14,
Space systems and operations.
Introduction
Throughout this International Standard, the minimum essential criteria are identified by the use of the key
word “shall”. Recommended criteria are identified by the use of the key word “should”, and while not
mandatory, are considered to be of primary importance in providing serviceable, economical and practical
designs. Deviations from the recommended criteria are only permissible after careful consideration, extensive
testing and thorough service evaluation have shown alternative methods to be satisfactory.
iv © ISO 2009 – All rights reserved
INTERNATIONAL STANDARD ISO 24637:2009(E)
Space systems — Electromagnetic interference (EMI) test
reporting requirements
1 Scope
This International Standard provides specific requirements for the content of equipment-level electromagnetic
interference (EMI) test report documentation to ensure that sufficient data is provided for subsequent
integration analysis of complex space systems. Emphasis is placed on necessary test report augmentation to
include additional test data reporting when specifically needed to document any EMI test limit failures for
spaceflight hardware.
The requirements presented in this International Standard apply only to EMI test reports at the equipment
level. These requirements are particularly important when an EMI test limit non-conformance waiver is
requested for spaceflight equipment in lieu of re-design.
2 Normative references
The following referenced documents are indispensable for the application 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 14302, Space systems — Electromagnetic compatibility requirements
ISO 15864, Space systems — General test methods for space craft, subsystems and units
ISO/IEC 17025:2005, General requirements for the competence of testing and calibration laboratories
3 Terms, definitions and abbreviated terms
3.1 Terms and definitions
For the purposes of this document, the following terms and definitions apply.
3.1.1
degradation criteria
minimum performance criteria required for acceptance of the product as specified in the electromagnetic
interference test plan
3.1.2
hard upset
degradation of product performance that requires manual (non-automatic) issuance of a reset command or
intervening procedure to restore product nominal performance without removal from the system
3.1.3
onset of susceptibility
degradation in product performance of at least one functional characteristic beyond equipment under test
parameter tolerance
3.1.4
product specification
equipment under test functional minimum performance requirements with associated accuracy parameters
3.1.5
soft upset
degradation in product performance where that product returns to normal with no operator intervention
immediately following the removal of the immunity test stimulus
3.2 Abbreviated terms
EMI electromagnetic interference
EMC electromagnetic compatibility
EUT equipment under test
IF intermediate frequency
LISN line impedance stabilization network
NE network equivalent
4 Equipment-level EMI test reporting requirements
4.1 General reporting requirements
4.1.1 General
The general content of the EMI test report shall be in accordance with ISO/IEC 17025:2005, 5.10.
System-level electromagnetic compatibility (EMC) test reporting shall comply with ISO 15864 and ISO 14302.
4.1.2 Description of the test article
The test article shall be identified by model and serial number. A short functional description of the EUT shall
be provided to enable the EMC systems analyst to understand the criticality of function, operating modes and,
if known, the significance of interfaces with other equipment in the complete operating system.
This requirement may be met with an associated reference which includes the equipment’s functional design
description, containing an explanation of nominal signal parameters such as data rate, clock speed, frequency
list, IF with bandwidths, and voltage input and output characteristics. A complete description of the test setup
shall be supplied in the form of photos and individual wiring harness schematics, including shielding, twisting
and grounding/isolation with respect to structure for primary power, secondary power and signal wiring
including that of external test loads.
It is expected that the EUT will be tested using cabling and connectors either pre-defined by the test method
or that agreed to by the customer, i.e. flight harness configuration. Any deviation from either standard test
method wiring configuration or flight harness configuration shall be noted in the test report. Setup, operation,
and control settings of any video display that is part of the EUT shall be described.
4.1.3 Supporting documentation
The standard(s) to which the EUT was tested shall be clearly described in the test report. The EMI test report
shall reference other supporting documentation containing the functional description and interface wiring, the
EMI test plan, EMI test specifications, techniques, “as run” procedures and the daily test log.
2 © ISO 2009 – All rights reserved
4.1.4 Signature information
The EMI test report shall contain the names of the EUT product engineer and the EMI test engineer, including
sufficient information so that they may be contacted by telephone or e-mail. The location of the test site shall
be identified in the test report.
4.1.5 Summary conclusions
The EMI test report shall contain a summary conclusion narrative, stating either complete compliance with
each of the EMI test requirements, or describing any non-conformance with the test limits or approved test
procedure, in such cases giving a list of non-conformance reports issued throughout the test.
4.1.6 Modifications to the EUT
A description shall be provided to explain any modification to the EUT during the course of performing the test
plan. It shall be made clear in the test report which corrective actions (modification of the EUT during the test)
will become part of the flight article, with those test results clearly marked as such.
4.1.7 Procedure variation
A description shall be provided to explain any modification to the test procedure during the course of
performing the test plan. Procedure variations shall be made clear in the test report to differentiate between
multiple test results, and clearly marked as such.
4.2 Specific reporting requirements
4.2.1 General
The test report shall contain:
a) all the information necessary to reproduce the test;
b) the EUT operating modes in which the emission and susceptibility tests have been performed.
4.2.2 EMI measurement system information
The following EMI measurement system detail shall be included in the EMI test report:
a) test equipment used, software support programme, and calibration certification;
b) photograph and drawings of each unique test setup, including EUT and interfacing cabling;
c) antenna factors and frequency ranges of magnetic and electric field antennas;
d) antenna distance from EUT;
e) transfer impedance of current probes and/or termination impedances provided by LISNs;
f) LISN (NE) transfer function as a function of frequency;
g) description of software operations/calculations used to produce measurement output (scan averaging or
peak-hold, antenna factors, cable loss, attenuators, and amplifiers): this description shall include the
means used to verify each test method’s end-to-end accuracy; if data quality has been compromised due
to test conditions, the reason and impact on results shall be stated;
h) measurement system scan speeds, step sizes, and measurement bandwidths as a function of frequency;
i) antenna polarizations used;
j) EUT power source frequency, voltage, nominal operating current, and facility temperature and relative
humidity;
k) compression level of active devices (amplifiers) in measurement chain;
l) facility limitations from that requested or required by the test plan and procedures;
m) method of radiated susceptibility field determination and modulation type;
n) grounding configuration of EUT and test support equipment.
4.2.3 EMI measurement reporting resolution
EMI test data shall be reported in graphic form with frequency resolution of 1 %, and decibel notation within
1 dB. For test limit failure conditions, improved data resolution shall be provided as further explained in 4.3.
4.3 Reporting emissions test results
4.3.1 General
Data output of the EUT test result shall be in the form of amplitude over time (for the time domain plots) and
amplitude over frequency (for frequency domain plots), superimposed with the EMI test limit. Conducted and
radiated interference background plots shall be included for each test configuration unless all emission data
are 6 dB below the limit. Test data shall include X and Y legend, date and time recorded and the respective
EUT operational mode.
4.3.2 Conducted interference test results
4.3.2.1 General
Each conducted interference test measurement result shall be clear in its intent to measure common-mode or
differential-mode current or voltage.
4.3.2.2 Power bus conducted interference, load induced, frequency domain
Data presentation shall be a graphic output of amplitude versus frequency. Units of measurement for
frequency domain conducted emissions measurements shall be reported in units of dB referenced to one
microvolt (dBuV), or referenced to one microampere (dBuA), depending on which transducer is specified by
the test method and its associated limit.
4.3.2.3 Power bus conducted interference, load induced, time domain ripple
Data presentation shall be a graphic output of amplitude versus time, at a time base that best displays the
voltage ripple frequency. Oscilloscope plots shall include the amplitude physical unit (V or A) conversion
factors V into A, if applicable, and the oscilloscope sensitivity, time base settings and measurement bandwidth.
Amplitude resolution shall be within 3 % and time base within 5 %.
4.3.2.4 Power bus load induced switching transients
Data presentation shall be a graphic display of voltage amplitude versus time, or current versus time for in-
rush at a time base that best displays the transient characteristic with respect to the applicable limit. Amplitude
resolution shall be within 3 % and time base within 5 %.
4 © ISO 2009 – All rights reserved
4.3.2.5 Antenna connection port spurious emissions
4.3.2.5.1 Receivers and transmitters (in standby mode)
Data presentation shall be a graphic output of amplitude versus frequency. Minimum frequency resolution
shall be twice the measurement receiver bandwidth, with a minimum amplitude resolution of 1 dB for each
graph.
4.3.2.5.2 Transmitters (in transmit mode)
Data presentation shall be graphical, indicating power amplitude within ±1 dB for fundamental transmit
frequency, and frequencies of all harmonics and spurious emissions detected by the app
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