ISO 14302-2022 PDF
Name in English:
St ISO 14302-2022
Name in Russian:
Ст ISO 14302-2022
Original standard ISO 14302-2022 in PDF full version. Additional info + preview on request
Full title and description
St ISO 14302-2022 — Space systems — Electromagnetic compatibility requirements. This International Standard defines a process to establish performance requirements and engineering controls to ensure electromagnetic compatibility (EMC) of space systems, and provides guidance for deriving equipment-level requirements from system-level EMC objectives and for tailoring requirements to a specific mission.
Abstract
This document sets out an engineering process and rationale for achieving system-level EMC for spacecraft and related space systems. It identifies the key EMC issues to be addressed during system design and integration, illustrates how to derive typical equipment-level requirements from a system-level EMC requirement, and provides guidance for selecting and tailoring requirements for particular missions (including informative material in an annex).
General information
- Status: Published
- Publication date: 15 June 2022
- Publisher: International Organization for Standardization (ISO)
- ICS / categories: 49.140 (Space systems and operations); 33.100.01 (Electromagnetic compatibility in general)
- Edition / version: Edition 2 (2022)
- Number of pages: 46
Scope
ISO 14302:2022 applies to space systems and describes a process to establish EMC performance requirements at system level, and to derive and tailor equipment- and subsystem-level requirements consistent with those system-level objectives. The standard is intended to be used during system definition, design, verification planning and integration to ensure electromagnetic compatibility across spacecraft, payloads and supporting ground or launch elements.
Key topics and requirements
- Framework and process for establishing system-level EMC performance requirements.
- Identification of engineering issues affecting system EMC (emissions, susceptibility, coupling paths, grounding/bonding, shielding, wiring and interfaces).
- Methodology to derive typical equipment- and subsystem-level requirements from system-level EMC requirements.
- Guidance on tailoring requirements for specific missions, including trade-offs and mission-specific threat assessment.
- Recommendations for verification planning, test allocation and documentation to demonstrate compliance with EMC requirements.
- Informative annex material illustrating tailoring examples and rationale.
Typical use and users
ISO 14302:2022 is used by spacecraft systems engineers, EMC engineers, payload integrators, test laboratories, prime contractors and mission assurance teams involved in the design, verification and integration of satellites, launch vehicle payloads and related space systems. It is a reference when defining EMC control plans, verification strategies and when translating system EMC objectives into equipment-level specifications.
Related standards
Typical related documents and normative references include the previous edition ISO 14302:2002 (superseded), applicable ECSS (European Cooperation for Space Standardization) EMC documents (for example ECSS-E-ST-20 family and ECSS-E-ST-20-07), general EMC series such as IEC 61000 (for laboratory and component EMC test methods), and other national/military EMC standards used by some projects (for example MIL-STD-461 where applicable). Project teams commonly use ISO 14302 together with organization-specific EMC control plans and ECSS guidance when working on space missions.
Keywords
space systems; electromagnetic compatibility; EMC; emissions; susceptibility; immunity; system-level requirements; equipment-level requirements; verification; tailoring; EMC control plan
FAQ
Q: What is this standard?
A: ISO 14302:2022 is an international standard titled "Space systems — Electromagnetic compatibility requirements" that defines a process and guidance for establishing and demonstrating EMC for space systems.
Q: What does it cover?
A: It covers the process for setting system-level EMC performance requirements, identifying engineering issues, deriving equipment- and subsystem-level requirements, and tailoring requirements and verification plans for specific missions (including illustrative annex material).
Q: Who typically uses it?
A: Systems and EMC engineers, spacecraft and payload integrators, test laboratories, mission assurance and technical leads on satellite and launch vehicle projects use the standard to define EMC requirements and verification strategies.
Q: Is it current or superseded?
A: ISO 14302:2022 is the current edition, published 15 June 2022; it supersedes ISO 14302:2002.
Q: Is it part of a series?
A: The standard is produced under ISO technical committee work for space systems (ISO/TC 20/SC 14) and is commonly used alongside related ECSS EMC standards and broader IEC/ISO EMC publications; it forms part of the body of standards and guidance used for space system engineering and EMC control.
Q: What are the key keywords?
A: Space systems, EMC, electromagnetic compatibility, emissions, immunity, verification, tailoring, system-level requirements, equipment-level requirements.