Romsystemer og drift

Komité: ISO/TC 20/SC 14 (Space systems and operations)
Opprinnelse: ISO
Sluttdato: 20. feb 2023
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ISO 17666:2016 defines, extending the requirements of ISO 14300‑1, the principles and requirements for integrated risk management on a space project. It explains what is needed to implement a project-integrated risk management policy by any project actor, at any level (i.e. customer, first-level supplier, or lower-level suppliers).


It contains a summary of the general risk management process, which is subdivided into four (4) basic steps and nine (9) tasks. The implementation can be tailored to project-specific conditions.


The risk management process requires information exchange among all project domains and provides visibility over risks, with a ranking according to their criticality for the project; these risks are monitored and controlled according to the rules defined for the domains to which they belong.


The fields of application of ISO 17666:2016 are all the space project phases. A definition of project phasing is given in ISO 14300‑1.


When viewed from the perspective of a specific programme or project context, the requirements defined in ISO 17666:2016 are tailored to match the genuine requirements of a particular profile and circumstances of a programme or project.

Komité: ISO/TC 20/SC 14 (Space systems and operations)
Opprinnelse: ISO
Sluttdato: 21. feb 2023
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ISO 27025:2010 defines the quality assurance (QA) requirements for the establishment and implementation of QA programmes for projects covering mission definition, design, development, production and operations of space systems, including disposal.


It is applicable to the customer-supplier relationship for space products to the extent agreed by both parties. The requirements of this International Standard and its associated referenced standards are tailored to the needs and classes of specific projects.


When viewed from the perspective of a specific project context, the requirements defined in ISO 27025:2010 are tailored to match the genuine requirements of a particular profile and circumstances of a project.


Komité: ISO/TC 20/SC 14 (Space systems and operations)
Opprinnelse: ISO
Sluttdato: 22. feb 2023
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ISO 27026:2011 specifies processes, requirements and recommendations for the breakdown of project management structures, collectively called project breakdown structures, in terms of the various specification (i.e. requirements), functional, product, work, cost, business and organizational breakdown structures that are established and implemented to contribute to the success of a space programme, which is often composed of one or more projects.


It is intended to complement and supplement similar project breakdown structure processes, requirements and recommendations contained within ISO 14300-1, which serves as a higher tier International Standard for ISO 27026:2011 and for such other space systems and operations International Standards that require formal project breakdown structures.


ISO 27026:2011 specifies the various types of project breakdown structures and gives processes, requirements and guidance concerning the composition of these breakdown structures.


ISO 27026:2011 is applicable to project breakdown structures for a project, including at the top level of a programme, i.e. level 0. It is intended to be used either by an independent developer as a partial basis for programme processes or as a basis for an agreement between a supplier and a customer.

Komité: CEN/CLC/JTC 5 (Space)
Opprinnelse: SN
Sluttdato: 23. mar 2023
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This activity w ill be the parallel development of EN 16603-20-40 and ECSS-E-ST-20-40C. The scope shall cover the areas of existing ASIC and FPGA engineering chapter 5 of ECSS-Q-ST-60-02C, but w ith w ider breadth and greater depth, covering engineering requirements of end-to-end development flow s, from specification of requirements to validation of prototypes, of the follow ing monolithic devices for its use in space: • ASICs (distinguishing digital, analogue and mixed-signal development flow s) • FPGAs (distinguishing three technology families: SRAM, FLASH and anti-fuse technologies) • ASIC and FPGA System-on-Chip embedding processor cores w hich have external “softw are programme” dependencies to be addressed during the SoC development, resulting in SW-HW co-design requirements.
Komité: ISO/TC 20/SC 14 (Space systems and operations)
Opprinnelse: ISO
Sluttdato: 28. mar 2023
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This International Standard defines the general criteria for the development of flight-to-ground umbilical systems


used by a space system. The criteria specified herein is limited to the service arms or equivalent mechanisms,


umbilical carriers and plates, couplings, connectors, withdrawal and retract devices, handling mechanisms and


control systems for mechanisms.