EN 16603-20-07:2014
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Space engineering - Electromagnetic compatibility
01-31-2015
07-09-2014
Foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
4 Requirements
5 Verification
Annex A (informative) - Subsystem and equipment
limits
Bibliography
EMC policy and general system requirements are specified in ECSS-E-ST-20.This ECSS-E-ST-20-07 Standard addresses detailed system requirements (Clause 4), general test conditions, verification requirements at system level, and test methods at subsystem and equipment level (Clause 5) as well as informative limits (Annex A).Associated to this standard is ECSS-E-ST-20-06 “Spacecraft charging”, which addresses charging control and risks arising from environmental and vehicle-induced spacecraft charging when ECSS-E-ST-20-07 addresses electromagnetic effects of electrostatic discharges.Annexes A to C of ECSS-E-ST-20 document EMC activities related to ECSS E ST 20 07: the EMC Control Plan (Annex A) defines the approach, methods, procedures, resources, and organization, the Electromagnetic Effects Verification Plan (Annex B) defines and specifies the verification processes, analyses and tests, and the Electromagnetic Effects Verification Report (Annex C) document verification results. The EMEVP and the EMEVR are the vehicles for tailoring this standard.This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Committee |
CEN/CLC/JTC 5
|
DocumentType |
Standard
|
PublisherName |
Comite Europeen de Normalisation
|
Status |
Withdrawn
|
Standards | Relationship |
DS EN 16603-20-07 : 2014 | Identical |
ONORM EN 16603-20-07 : 2014 | Identical |
NF EN 16603-20-07 : 2016 | Identical |
UNE-EN 16603-20-07:2014 | Identical |
DIN EN 16603-20-07:2014-09 | Identical |
NS EN 16603-20-07 : 2014 | Identical |
CEI UNI EN 16603-20-07 : 1ED 2016 | Identical |
UNI EN 16603-20-07 : 2014 | Identical |
PN EN 16603-20-07 : 2014 | Identical |
BS EN 16603-20-07:2014 | Identical |
I.S. EN 16603-20-07:2014 | Identical |
NEN EN 16603-20-07 : 2014 | Identical |
PNE-FprEN 16603-20-07 | Identical |
BS EN 16603-50-15:2017 | Space engineering. CANbus extention protocol |
I.S. EN 16603-10-03:2014 | SPACE ENGINEERING - TESTING |
BS EN 16603-35-01:2014 | Space engineering. Liquid and electric propulsion for spacecraft |
I.S. EN 16603-35-01:2014 | SPACE ENGINEERING - LIQUID AND ELECTRIC PROPULSION FOR SPACECRAFT |
UNI EN 16603-20-06 : 2014 | SPACE ENGINEERING - SPACECRAFT CHARGING |
16/30340717 DC : 0 | BS EN 16603-50-15 - SPACE ENGINEERING - CANBUS EXTENTION PROTOCOL |
BS EN 16603-10-03:2014 | Space engineering. Testing |
I.S. EN 16603-35-02:2014 | SPACE ENGINEERING - SOLID PROPULSION FOR SPACECRAFTS AND LAUNCHERS |
EN 16603-20-06:2014 | Space engineering - Spacecraft charging |
BS EN 16603-20-06:2014 | Space engineering. Spacecraft charging |
I.S. EN 16603-50-15:2017 | SPACE ENGINEERING - CANBUS EXTENTION PROTOCOL |
EN 16603-50-15:2017 | Space engineering - CANbus extention protocol |
EN 16603-35-02:2014 | Space engineering - Solid propulsion for spacecrafts and launchers |
EN 16603-35-01:2014 | Space engineering - Liquid and electric propulsion for spacecraft |
EN 16603-10-03:2014 | Space engineering - Testing |
BS EN 16603-35-02:2014 | Space engineering. Solid propulsion for spacecrafts and launchers |
I.S. EN 16603-20-06:2014 | SPACE ENGINEERING - SPACECRAFT CHARGING |
MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
EN 16601-00-01:2015 | Space systems - Glossary of terms |
IEC 61000-4-2:2008 | Electromagnetic compatibility (EMC) - Part 4-2: Testing and measurement techniques - Electrostatic discharge immunity test |
EN 16603-50-14:2014 | Space engineering - Spacecraft discrete interfaces |
EN 16603-20-06:2014 | Space engineering - Spacecraft charging |
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