This Standard specifies star sensor performances as part of a space project. The Standard covers all aspects of performances, including nomenclature, definitions, and performance requirements for the performance specification of star sensors.
The Standard focuses on:
- performance specifications (including the impact of temperature, radiation and straylight environments);
- robustness (ability to maintain functionalities under non nominal environmental conditions).
Other specification types, for example mass and power, housekeeping data and data structures, are outside the scope of this Standard.
This Standard also proposes a standard core of functional interfaces defined by unit suppliers and avionics primes in the context of Space AVionics Open Interface aRchitecture (SAVOIR) initiative.
When viewed from the perspective of a specific project context, the requirements defined in this Standard should be tailored to match the genuine requirements of a particular profile and circumstances of a project.
This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.

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This document defines terms and definitions relating to unmanned aircraft systems that are widely used in science and technology.

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This document provides definitions of all common terms used in the area of space systems and operations for programme management and quality. It does not contain terms specific to an individual International Standard in the area of space systems and operations, which are defined in that particular International Standard.

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This Standard specifies gyros functions and performances as part of a space project. This Standard covers aspects of functional and performance requirements, including nomenclature, definitions, functions and performance metrics for the performance specification of spaceborne gyros.
The Standard focuses on functional and performance specifications with the exclusion of mass and power, TM/TC interface and data structures.
When viewed from the perspective of a specific project context, the requirements defined in this Standard can be tailored to match the genuine requirements of a particular profile and circumstances of a project.
The requirements verification by test can be performed at qualification level only or also at acceptance level. It is up to the Supplier, in agreement with the customer, to define the relevant verification approach in the frame of a specific procurement, in accordance with clause 5.2 of ECSS-E-ST-10-02.
The present standard does not cover gyro use for launch vehicles.
This standard can be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.

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This Standard specifies gyros functions and performances as part of a space project. This Standard covers aspects of functional and performance requirements, including nomenclature, definitions, functions and performance metrics for the performance specification of spaceborne gyros.
The Standard focuses on functional and performance specifications with the exclusion of mass and power, TM/TC interface and data structures.
When viewed from the perspective of a specific project context, the requirements defined in this Standard can be tailored to match the genuine requirements of a particular profile and circumstances of a project.
The requirements verification by test can be performed at qualification level only or also at acceptance level. It is up to the Supplier, in agreement with the customer, to define the relevant verification approach in the frame of a specific procurement, in accordance with clause 5.2 of ECSS-E-ST-10-02.
The present standard does not cover gyro use for launch vehicles.
This standard can be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.

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This document explains the wording in use within the following standards:
EN 9223-100, Programme Management — Configuration Management — Part 100: A guide for the
application of the principles of configuration management
EN 9223-101, Programme Management — Configuration Management — Part 101: Configuration
identification
EN 9223-102, Programme Management — Configuration Management — Part 102: Configuration status
accounting
EN 9223-103, Programme Management — Configuration Management — Part 103: Configuration
Verifications, Reviews and Audits
EN 9223-104, Programme Management — Configuration Management — Part 104: Configuration
Control

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ISO 8625-1:2018 defines general terms relating to pressure in fluid systems used in aerospace construction.

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ISO 8625-2:2018 defines general terms relating to flow in fluid systems used in aerospace construction.

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ISO 8625-3:2018 defines general terms relating to temperature in fluid systems used in aerospace construction.

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This document explains the wording in use within the following standards:
EN 9223-100, Programme Management - Configuration Management - Part 100: A guide for the application of the principles of configuration management
EN 9223-101, Programme Management - Configuration Management - Part 101: Configuration identification
EN 9223-102, Programme Management - Configuration Management - Part 102: Configuration status accounting
EN 9223-103, Programme Management - Configuration Management - Part 103: Configuration Verifications, Reviews and Audits
EN 9223 -04, Programme Management - Configuration Management - Part 104: Configuration Control

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This document controls the definition of all common terms used in the European Cooperation for Space Standardization (ECSS) Standards System. Terms specific to a particular ECSS Standard are defined in that standard.
This document does not include the definition of terms used with their common meaning. In this case, the definition from the Oxford English Dictionary applies.

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This document controls the definition of all common terms used in the European Cooperation for Space Standardization (ECSS) Standards System. Terms specific to a particular ECSS Standard are defined in that standard.
This document does not include the definition of terms used with their common meaning. In this case, the definition from the Oxford English Dictionary applies.

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ISO 18542 is structured in two parts:
Part 1 defines a framework and a process for agreeing terms;
Part 2 defines the process implementation requirements for a terminology management system and for a Registration Authority with a digital annex.
The basic purpose of ISO 18542 is to facilitate searching of vehicle manufacturer (VM) repair and maintenance information (RMI) websites by independent operators (IOs).
ISO 18542-1:2012 provides a general overview and structure of each part of ISO 18542. It also specifies use cases related to repair and maintenance information (RMI) terminology in order to standardize the access to RMI for IOs.
The provision of the agreed automotive RMI terminology itself is outside the remit of ISO 18542 and therefore outside the scope of ISO 18542-1:2012. Rather, it is foreseen that the agreed automotive RMI terminology will follow a lifecycle beyond the timeframe of ISO 18542. It will be dependent upon the work of a Registration Authority, a Terminology Review Group for its creation and management, and of a digital annex for its publication. For the development of the digital annex, existing standards will be reviewed and elements included where appropriate and practical.

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ISO 8625-4:2011 defines general terms relating to control/actuation systems in the field of aerospace fluid systems and components.

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ISO 8153-1:2009 defines terms used for all types of hose assemblies. General terms can be made more precise through the addition of supplementary terminology relating to the design, range of application and/or the material of the hose/hose assembly. Terms and definitions specific to metallic hose assemblies are given in ISO 7369.

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This Standard specifies star sensor performances as part of a space project. The Standard covers all aspects of performances, including nomenclature, definitions, and performance requirements for the performance specification of star sensors.
The Standard focuses on:
- performance specifications (including the impact of temperature, radiation and straylight environments);
- robustness (ability to maintain functionalities under non nominal environmental conditions).
Other specification types, for example mass and power, housekeeping data and data structures, are outside the scope of this Standard.
This Standard also proposes a standard core of functional interfaces defined by unit suppliers and avionics primes in the context of Space AVionics Open Interface aRchitecture (SAVOIR) initiative.
When viewed from the perspective of a specific project context, the requirements defined in this Standard should be tailored to match the genuine requirements of a particular profile and circumstances of a project.
This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.

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    208 pages
    Slovenian and English language
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This European Standard contains the definition of all common terms used in European space standards. Terms specific to a particular space standard are defined in that standard.

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This European Standard contains the definition of all common terms used in European space standards. Terms specific to a particular space standard are defined in that standard.

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ISO 10795:2011 provides definitions of all common terms used in the area of space systems and operations. ISO 10795:2011does not contain terms specific to an individual International Standard in the area of space systems and operations, which are defined in that particular International Standard.

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