| Name |
Description |
Abstract |
Status |
Publication date |
Edition |
Number of pages |
Technical committee |
ICS |
| ISO 11104:2011 |
Space data and information transfer systems — Time code formats |
ISO 11104:2011 establishes a small number of standardized recommended time code formats for use in data interchange applications between agencies of the CCSDS. ISO 11104:2011 does not address timing performance issues such as stability, precision, accuracy, etc.
Time codes are digital representations of time information. ISO 11104:2011 describes four standard recommended time codes (one "unsegmented" and three "segmented" codes) which use the international standard second as the fundamental unit of time. An unsegmented time code is a pure binary count of time units and fractional time units from a starting time called the "epoch". A segmented time code is one in which the count of time units and fractional time units is accumulated in two or more cascaded counters which count modulo of various bases and start from the epoch.
|
Published |
2011-12 |
Edition : 3 |
Number of pages : 51 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 12172:1998 |
Space data and information transfer systems — Telecommand — Data routing service |
|
Withdrawn |
1998-09 |
Edition : 1 |
Number of pages : 58 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/TR 11225:2012 |
Space environment (natural and artificial) — Guide to reference and standard atmosphere models |
ISO/TR 11225:2012 provides guidelines for selected reference and standard atmospheric models for use in engineering design or scientific research. It describes the content of the models, uncertainties and limitations, technical basis, databases from which the models are formed, publication references, and sources of computer code where available for over seventy (70) Earth and planetary atmospheric models, for altitudes from surface to 4 000 km, which are generally recognized in the aerospace sciences. ISO/TR 11225:2012 is intended to assist aircraft and space vehicle designers and developers, geophysicists, meteorologists, and climatologists in understanding available models, comparing sources of data, and interpreting engineering and scientific results based on different atmospheric models.
ISO/TR 11225:2012 summarizes the principal features of the models to the extent the information is available:
- model content;
- model uncertainties and limitations;
- basis of the model;
- publication references;
- dates of development, authors and sponsors;
- model codes and sources.
|
Published |
2012-10 |
Edition : 1 |
Number of pages : 107 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 11227:2012 |
Space systems — Test procedure to evaluate spacecraft material ejecta upon hypervelocity impact |
ISO 11227:2012 describes an experimental procedure for assessing the behaviour, under orbital debris or meteoroid impacts, of materials that are intended to be used on the external surfaces of spacecraft and launch vehicle orbital stages. ISO 11227:2012 provides a unified method by which to rank materials. The ejecta production characteristics of different materials are compared under standardized conditions in which test parameters are fixed to one number. Optional tests with different parameters are also useful for the proper selection of materials in other conditions, and they could be performed as research items.
ISO 11227:2012 establishes the requirements to be satisfied for the test methods in order to characterize the amount of ejecta produced when a surface material is impacted by a hypervelocity projectile. Its purpose is to evaluate the ratio of ejecta total mass to projectile mass, and the size distribution of the fragments. These are the necessary inputs for modelling the amount of impact ejecta that a surface material might release during its orbital lifetime, thereby helping to assess its suitability for space use while mitigating the production of small space debris.
The purpose of ISO 11227:2012 is to provide data that need to be taken into account in the selection of outer spacecraft materials, though the selection is not based on these criteria alone.
The experimental procedure defines
the type of facility to be used,
the size, velocity and type of projectile to be used,
the evaluation of impact ejecta released,
the reporting of test results, and
the quality requirements to be used.
ISO 11227:2012 is applicable to spacecraft and launch vehicles operating in all types of Earth orbits.
|
Published |
2012-09 |
Edition : 1 |
Number of pages : 23 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 11227:2012/Amd 1:2021 |
Space systems — Test procedure to evaluate spacecraft material ejecta upon hypervelocity impact — Amendment 1: Oblique impacts and Annex C update |
|
Published |
2021-01 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 11231:2010 |
Space systems — Probabilistic risk assessment (PRA) |
ISO 11231:2010 supports and complements the implementation of the risk management process defined in ISO 17666 in situations when application of quantitative risk assessment is deemed necessary.
ISO 11231:2010 defines the principles, process, implementation and requirements for conducting a quantitative risk assessment, and explains the details of probabilistic risk assessment (PRA) as applied to safety. While PRA can be applied to project risk management involving cost and schedule, this application is outside the scope of ISO 11231:2010.
ISO 11231:2010 provides the basic requirements and procedures for use of PRA techniques to assess safety or mission risk and success in space programmes and projects. ISO 11231:2010 is applicable to all international space projects involving:
the design of space vehicles for the transportation of personnel in space;
the design of space and non-terrestrial planetary stations inhabited by human beings;
the design of space and launch vehicles powered by, or carrying, nuclear materials;
other projects as directed by authorities or clients.
These types of projects generally involve scenarios, chains of events or activities that could result in the death of, or serious injury to, members of the public, astronauts or pilots, or the workforce, or the loss of critical or high-value equipment and property. For other types of projects, it is intended that PRA be performed at the discretion of the project management.
|
Withdrawn |
2010-08 |
Edition : 1 |
Number of pages : 17 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 11231:2019 |
Space systems — Probabilistic risk assessment (PRA) |
This document supports and complements the implementation of the risk management process defined in ISO 17666 in situations when the application of a quantitative risk assessment is deemed necessary.
This document defines the principles, process, implementation and requirements for conducting a quantitative risk assessment and explains the details of probabilistic risk assessment (PRA) as applied to safety. While PRA can be applied to project risk management involving cost and schedule, this application is outside the scope of this document.
This document provides the basic requirements and procedures for the use of PRA techniques to assess safety or mission risk and success in space programmes and projects. This document is applicable to all international space projects involving:
— the design of space vehicles for the transportation of personnel in space;
— the design of space and non-terrestrial planetary stations inhabited by human beings;
— the design of space and launch vehicles powered by, or carrying, nuclear materials;
— other projects as directed by the authorities or clients.
These types of projects generally involve scenarios, chains of events or activities that could result in the death of, or serious injury to, members of the public, astronauts or pilots, or the workforce, or the loss of critical or high-value equipment and property. For other types of projects, it is intended that PRA be performed at the discretion of the project management.
|
Published |
2019-05 |
Edition : 2 |
Number of pages : 22 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14951-3:1999 |
Space systems — Fluid characteristics — Part 3: Nitrogen |
|
Withdrawn |
1999-09 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/TR 11233:2014 |
Space systems — Orbit determination and estimation — Process for describing techniques |
ISO/TR 11233:2014 prescribes the manner in which orbit determination and estimation techniques are to be described so that parties can plan operations with sufficient margin to accommodate different individual approaches to orbit determination and estimation. ISO/TR 11233:2014 does not require the exchange of orbit data nor does it prescribe a method of performing orbit determination. It only prescribes the information that shall accompany such data so that collaborating satellite owners/operators understand the similarities and differences between their independent orbit determination processes.
All satellite owners/operators are entitled to a preferred approach to physical approximations, numerical implementation, and computational execution of orbit determination and estimation of future states of their satellites. Mission demands should determine the architecture (speed of execution, required precision, etc.). ISO/TR 11233:2014 will enable stakeholders to describe their techniques in a manner that is uniformly understood. Implementation details that can have proprietary or competitive advantage need not be revealed.
|
Published |
2014-04 |
Edition : 1 |
Number of pages : 19 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 11754:1994 |
Space data and information transfer systems — Telemetry channel coding |
Specifies the requirements for telemetry channel coding for space date and information transfer systems for civil space applications.
|
Withdrawn |
1994-10 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 11754:2003 |
Space data and information transfer systems — Telemetry channel coding |
ISO 11754:2003 specifies the requirements for telemetry channel coding of space data and information transfer systems used in civil space applications.
|
Withdrawn |
2003-02 |
Edition : 2 |
Number of pages : 65 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 11892:2012 |
Space systems — Subsystems/units to spacecraft interface control document |
This International Standard provides space system manufacturing organizations with the minimum interface related items and generic format for creating the interface control document (ICD) which subsystems or units suppliers prepare for spacecraft systems (SC) integrators. In this International Standard, ICD is not defined to contain descriptions regarding various properties of subsystems or units or tasks to be done by suppliers, i.e. performance, functions, endurance to launch mechanical environment, or quality assurance provisions. Such descriptions are presumed to be defined in other contractual documents such as technical specifications.
|
Published |
2012-03 |
Edition : 1 |
Number of pages : 16 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/CD 11892 |
Space systems — Subsystems/units to spacecraft interface control document |
This International Standard provides space system manufacturing organizations with the minimum interface related items and generic format for creating the interface control document (ICD) which subsystems or units suppliers prepare for spacecraft systems (SC) integrators. In this International Standard, ICD is not defined to contain descriptions regarding various properties of subsystems or units or tasks to be done by suppliers, i.e. performance, functions, endurance to launch mechanical environment, or quality assurance provisions. Such descriptions are presumed to be defined in other contractual documents such as technical specifications.
|
Under development |
|
Edition : 2 |
|
Technical Committee |
49.140
Space systems and operations
|
| ISO 11893:2011 |
Space systems — Programme management — Project organization |
ISO 11893:2011 defines the project organization principles and requirements needed to provide satisfactory and coherent management of space projects.
The general requirements for project organization are given in ISO 14300-1.
It addresses the following, in particular:
responsibility and authority of the actors (all actors, customer, supplier),
interrelations between the actors (meetings, action monitoring, reporting, assessments and audits),
information technologies, and
project organization documentation.
The requirements specified herein apply to and affect the supplier and customer at all levels.
ISO 11893:2011 is applicable to the customer-supplier relationship for space products to the extent agreed by both parties. It is intended to be used as a basis when establishing and negotiating customer program/project management requirements and to guide the supplier's responses. When viewed in a specific project context, the requirements defined in this International Standard should be tailored to match the specific requirements of a particular profile and circumstances of a project.
|
Published |
2011-04 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 12171:1998 |
Space data and information transfer systems — Telecommand — Channel service — Architectural specification |
|
Withdrawn |
1998-07 |
Edition : 1 |
Number of pages : 46 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 12171:2002 |
Space data and information transfer systems — Telecommand — Channel service |
ISO 12171:2002 specifies the common requirements which define the systems architecture of a spacecraft telecommand channel service. This architecture is intended to provide a common framework within which space agencies may implement compatible future spacecraft telecommanding systems.
ISO 12171:2002 establishes a layered concept for spacecraft telecommanding. Standard services are defined within each layer, and space agencies will be encouraged to develop corresponding facilities to provide these services in support of projects. Projects may also elect to be partially compatible with the concept by interfacing with the standard systems at intermediate layers within any of the service specifications.
|
Withdrawn |
2002-09 |
Edition : 2 |
Number of pages : 49 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 12174:2003 |
Space data and information transfer systems — Telecommand — Architectural specification for the data management service |
ISO 12174:2003 specifies the requirements, which define the architecture of a spacecraft telecommand data management service. This architecture is intended to provide a common framework within which space agencies may implement compatible future spacecraft telecommanding systems.
ISO 12174:2003 primarily addresses the data unit formats and functions, which are implemented within the application process layer, the system management layer and the packetization layer of the CCSDS telecommand data management service.
|
Withdrawn |
2003-02 |
Edition : 2 |
Number of pages : 59 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 12175:1994 |
Space data and information transfer systems — Standard formatted data units — Structure and construction rules |
Lays down the requirements for structure and construction rules for standard formatted data units for space data and information transfer systems.
|
Published |
1994-11 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 12175:1994/Amd 1:2015 |
Space data and information transfer systems — Standard formatted data units — Structure and construction rules — Amendment 1 |
|
Published |
2015-07 |
Edition : 1 |
Number of pages : 53 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 12208:2015 |
Space systems — Space environment (natural and artificial) — Observed proton fluences over long duration at GEO and guidelines for selection of confidence level in statistical model of solar proton fluences |
ISO 12208:2015 describes a method to estimate energetic proton fluences in geosynchronous earth orbit (GEO) over a long duration (beyond the 11-year solar cycle), and presents guidelines for the selection of a confidence level in a model of solar proton fluences to estimate solar cell degradation.
Many of the proton data observed in GEO are archived, for example from GMS (Japan), METEOSAT (ESA) and GOES (USA). This method is a direct integration of these fluence data (or the observed data over 11 years is used periodically).
As a result, the confidence level can be selected from a model of solar proton fluences.
ISO 12208:2015 is an engineering-oriented method used for specific purposes such as estimating solar panel degradation.
|
Published |
2015-10 |
Edition : 1 |
Number of pages : 9 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/TS 12208:2011 |
Space systems — Space environment (natural and artificial) - Observed proton fluences over long duration at GEO and guideline for selection of confidence level in statistical model of solar proton fluences |
ISO/TS 12208:2011 describes a method to estimate energetic proton fluences in geosynchronous earth orbit (GEO) over a long duration (beyond the 11-year solar cycle), and presents guidelines for the selection of a confidence level in a model of solar proton fluences to estimate solar cell degradation.
Many of the proton data observed in GEO are archived, for example GMS (Japan), METEOSAT (ESA) and GOES (USA). This method is a direct integration of these fluence data (or the observed data over 11 years is used periodically).
As a result, the confidence level can be selected from a model of solar proton fluences.
ISO/TS 12208:2011 is an engineering-oriented method used for specific purposes such as estimating solar panel degradation.
|
Withdrawn |
2011-09 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 13419:1997 |
Space data and information transfer systems — Packet telemetry |
|
Withdrawn |
1997-12 |
Edition : 1 |
Number of pages : 34 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 13419:2003 |
Space data and information transfer systems — Packet telemetry |
ISO 13419:2003 specifies the requirements for spacecraft packet telemetry systems. Packet telemetry is a concept which facilitates the transmission of space-acquired data from source to user in a standardized highly automated manner. Packet telemetry provides a mechanism for implementing common data transport structures and protocols, which may enhance the development and operation of space mission systems.
ISO 13419:2003 addresses two processes: the end-to-end transport of space mission data sets from source application processes located in space to distributed user application processes located on the ground, and the intermediate transfer of these data sets through space data acquisition networks, which contain spacecraft, radio links, tracking stations, ground communications circuits and mission control centres as some of their components.
ISO 13419:2003 is limited to describing the telemetry formats, which are generated by the spacecraft in order to execute its role in the above processes. It includes comprehensive specification of the structure of data streams that are generated by remote space vehicles for telemetering to space mission data processing facilities (which are usually located on Earth). It does not attempt to define the architecture or configuration of these data processing facilities, except to describe assumed ground data handling services, which affect the selection of certain on-board formatting options.
ISO 13419:2003 specifies a wide range of formatting capabilities, which may facilitate a high degree of flexibility in the design of spacecraft data acquisition systems; however, compatibility with the packet telemetry concept may be realized by only implementing a narrow subset of these capabilities.
|
Withdrawn |
2003-02 |
Edition : 2 |
Number of pages : 52 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 13420:1997 |
Space data and information transfer systems — Advanced orbiting systems — Networks and data links — Architectural specification |
|
Withdrawn |
1997-12 |
Edition : 1 |
Number of pages : 165 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14200:2012 |
Space environment (natural and artificial) — Guide to process-based implementation of meteoroid and debris environmental models (orbital altitudes below GEO + 2 000 km) |
This International Standard specifies the common implementation process for meteoroid and debris environment models for risk assessment of spacecraft and launch vehicle orbital stages. This International Standard gives guidelines for the selection process of models for impact risk assessment and ensures the traceability of using models throughout the design phase of a spacecraft or launch vehicle orbital stage.
|
Withdrawn |
2012-11 |
Edition : 1 |
Number of pages : 16 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 13526:2010 |
Space data and information transfer systems — Tracking data message |
ISO 13526:2010 specifies a standard message format for use in exchanging spacecraft tracking data between space agencies. Such exchanges are used for distributing tracking data output from routine interagency cross-supports, in which spacecraft missions managed by one agency are tracked from a ground station managed by a second agency. The standardization of tracking data formats facilitates space agency allocation of tracking sessions to alternate tracking resources.
ISO 13526:2010 includes requirements and criteria that the message format has been designed to meet. For exchanges where these requirements do not capture the needs of the participating agencies, another mechanism can be selected.
|
Published |
2010-09 |
Edition : 1 |
Number of pages : 80 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 13526:2010/Amd 1:2015 |
Space data and information transfer systems — Tracking data message — Amendment 1 |
|
Published |
2015-07 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 13527:2010 |
Space data and information transfer systems — XML formatted data unit (XFDU) structure and construction rules |
ISO 13527:2010 defines how the packaging of data and metadata, including software, can be put into a single package (e.g. file or message) in order to facilitate information transfer and archiving.
ISO 13527:2010 also provides a detailed specification of core packaging structures and mechanisms, which accommodate the current computing environment and meet evolving requirements, and which can be implemented to demonstrate practical, near-term results.
ISO 13527:2010 is applicable to the entire space informatics domain, from operational messaging to interfacing with science archives.
|
Published |
2010-09 |
Edition : 1 |
Number of pages : 69 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 13537:2010 |
Space data and information transfer systems — Reference architecture for space data systems |
ISO 13537:2010 presents a reference architecture for space data systems (RASDS). The RASDS is intended to provide a standardized approach for description of data system architectures and high-level designs, which individual CCSDS working groups may use within CCSDS. This approach is aligned with current practices in the fields of system and software architecture and is specifically adapted for the space domain. While it is intended for use within CCSDS, it is also suitable for use by mission and project design teams to describe system architectures and designs within the space domain. It does not propose any specific formal modeling method or tool, but can be adapted to use methods like UML or SysML.
|
Published |
2010-10 |
Edition : 1 |
Number of pages : 121 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 13541:2010 |
Space data and information transfer systems — Attitude data messages |
ISO 13541:2010 specifies two standard message formats for use in transferring spacecraft attitude information between space agencies: the attitude parameter message (APM) and the attitude ephemeris message (AEM). Such exchanges are used for: preflight planning for tracking or attitude estimation support; scheduling attitude and data processing support; carrying out attitude operations; performing attitude comparisons; carrying out attitude propagations and/or sensor predictions; and testing to initialize sub-system simulators (communications, power, etc.).
ISO 13541:2010 includes sets of requirements and criteria that the message formats have been designed to meet. For exchanges where these requirements do not capture the needs of the participating agencies, another mechanism may be selected.
|
Withdrawn |
2010-09 |
Edition : 1 |
Number of pages : 54 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 13541:2021 |
Space data and information transfer systems — Attitude data messages |
This document specifies two standard message formats for use in transferring spacecraft attitude information between space agencies: the Attitude Parameter Message (APM) and the Attitude Ephemeris Message (AEM). Such exchanges are used for:
- preflight planning for tracking or attitude estimation support;
- scheduling attitude and data processing support;
- carrying out attitude operations;
- performing attitude comparisons;
- carrying out attitude propagations and/or sensor predictions;
- testing to initialize sub-system simulators (communications, power, etc.).
This document includes sets of requirements and criteria that the message formats have been designed to meet. For exchanges where these requirements do not capture the needs of the participating agencies, another mechanism may be selected.
|
Published |
2021-06 |
Edition : 2 |
Number of pages : 52 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/CD 13657 |
Space systems — Space-based services — Positioning information exchange service |
This document specifies contents and formats of positioning information that is exchanged between appliances, features, and systems in motion or at rest, for safety, reliability and resilience of navigation. It is applied to onshore, maritime and aerial applications using space-based positioning and other sensing.
|
Under development |
|
Edition : 1 |
|
Technical Committee |
49.140
Space systems and operations
|
| ISO 13764:1996 |
Space data and information transfer systems — Standard formatted data units — Control authority procedures |
Lays down the requirements for Control Authority procedures for standard formatted data units used in space systems. Technically identical with CCSDS 630.0.B-1-1993.
|
Published |
1996-12 |
Edition : 1 |
Number of pages : 25 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14951-3:1999/Cor 1:2000 |
Space systems — Fluid characteristics — Part 3: Nitrogen — Technical Corrigendum 1 |
|
Withdrawn |
2000-09 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14200:2021 |
Space environment (natural and artificial) — Process-based implementation of meteoroid and debris environment models (orbital altitudes below GEO + 2 000 km) |
This document specifies a common process for selecting and implementing meteoroid and space debris environment models used in the impact flux assessment for design and operation of spacecraft and other purposes. This document provides guidelines and requirements for the process.
|
Published |
2021-06 |
Edition : 2 |
Number of pages : 14 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14222:2013 |
Space environment (natural and artificial) — Earth upper atmosphere |
ISO 14222:2013 specifies the structure of Earth's atmosphere above 120 km, provides accepted empirical models that can specify the details of the atmosphere, and uses annexes to describe the details of those models. Its purpose is to create a standard method for specifying Earth atmosphere properties (densities, etc.) in the low Earth orbit regime for space systems and materials users.
|
Withdrawn |
2013-09 |
Edition : 1 |
Number of pages : 38 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14222:2022 |
Space environment (natural and artificial) — Earth's atmosphere from ground level upward |
This document specifies the structure and properties of the Earth’s atmosphere from ground level upward. It provides internationally accepted empirical models that specify the details of the atmosphere. It also refers to widely-accepted physical models providing insight into the physical and chemical processes driving the response of the atmosphere.
|
Published |
2022-03 |
Edition : 2 |
Number of pages : 49 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14300-1:2001 |
Space systems — Programme management — Part 1: Structuring of a programme |
|
Withdrawn |
2001-05 |
Edition : 1 |
Number of pages : 31 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14300-1:2011 |
Space systems — Programme management — Part 1: Structuring of a project |
ISO 14300-1:2011 addresses the space programme/project management requirements, applicable through a top-down approach in a contractual relationship between customers and suppliers.
The applicable requirements for product assurance are given in ISO 14300-2. Annex A of ISO 14300-1:2011 gives the general ISO standards framework for space systems programme management.
ISO 14300-1:2011 is intended to be used as a basis when establishing and negotiating customer project management requirements, and guiding the supplier's responses.
It allows:
a clear definition of the roles, responsibilities and authorities of the different customers and suppliers;
coherence between their activities;
communication capability between them;
stable and rigorous project organization; and
as far as possible, standardization of the rules applicable to various programmess/projects.
It still allows for supplier flexibility in its implementation and tailoring.
|
Published |
2011-07 |
Edition : 2 |
Number of pages : 35 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/DIS 14300-1 |
Space systems — Programme management — Part 1: Structuring of a project |
ISO 14300-1:2011 addresses the space programme/project management requirements, applicable through a top-down approach in a contractual relationship between customers and suppliers.
The applicable requirements for product assurance are given in ISO 14300-2. Annex A of ISO 14300-1:2011 gives the general ISO standards framework for space systems programme management.
ISO 14300-1:2011 is intended to be used as a basis when establishing and negotiating customer project management requirements, and guiding the supplier's responses.
It allows:
a clear definition of the roles, responsibilities and authorities of the different customers and suppliers;
coherence between their activities;
communication capability between them;
stable and rigorous project organization; and
as far as possible, standardization of the rules applicable to various programmess/projects.
It still allows for supplier flexibility in its implementation and tailoring.
|
Under development |
|
Edition : 3 |
Number of pages : 35 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14300-2:2002 |
Space systems — Programme management — Part 2: Product assurance |
|
Withdrawn |
2002-07 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14300-2:2011 |
Space systems — Programme management — Part 2: Product assurance |
ISO 14300-2:2011 defines the product assurance (PA) policy, objectives, principles, and requirements for the establishment and implementation of PA programmes for space programmes covering mission definition, design, development, production and operations of space products, including disposal.
The PA discipline covers: PA management, quality assurance, safety assurance, dependability (reliability, availability and maintainability) assurance of software and hardware products, as well as parts (including electrical, electromechanical and electronic components, and mechanical parts), materials and processes assurance. ISO 14300-2:2011 defines their respective objectives, policies, and principles to achieve the stated overall PA objectives throughout the complete life cycle of the products.
The provisions of ISO 14300-2:2011 apply to space products.
|
Published |
2011-09 |
Edition : 2 |
Number of pages : 9 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14621-1:2019 |
Space systems — Electrical, electronic and electromechanical (EEE) parts — Part 1: Parts management |
This document addresses the key elements for an EEE parts management programme for space systems and is written in general terms as a baseline for developing, implementing, validating, and evaluating a space parts management programme. The family of EEE parts includes electro-optical parts.
|
Published |
2019-05 |
Edition : 2 |
Number of pages : 40 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/DIS 14300-2 |
Space systems — Programme management — Part 2: Product assurance |
ISO 14300-2:2011 defines the product assurance (PA) policy, objectives, principles, and requirements for the establishment and implementation of PA programmes for space programmes covering mission definition, design, development, production and operations of space products, including disposal.
The PA discipline covers: PA management, quality assurance, safety assurance, dependability (reliability, availability and maintainability) assurance of software and hardware products, as well as parts (including electrical, electromechanical and electronic components, and mechanical parts), materials and processes assurance. ISO 14300-2:2011 defines their respective objectives, policies, and principles to achieve the stated overall PA objectives throughout the complete life cycle of the products.
The provisions of ISO 14300-2:2011 apply to space products.
|
Under development |
|
Edition : 3 |
Number of pages : 10 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14302:2002 |
Space systems — Electromagnetic compatibility requirements |
ISO 14302:2002 establishes performance requirements for the purpose of ensuring space systems electromagnetic compatibility (EMC). The engineering issues to be addressed in order to achieve system-level EMC are identified herein, with guidance and rationale towards achieving specification conformance. The method for the derivation of typical equipment-level requirements from a space-system-level requirement is illustrated.
|
Withdrawn |
2002-12 |
Edition : 1 |
Number of pages : 49 |
Technical Committee |
49.140
Space systems and operations
;
33.100.01
Electromagnetic compatibility in general
|
| ISO 14302:2022 |
Space systems — Electromagnetic compatibility requirements |
This document contains a process to establish performance requirements for the purpose of ensuring space systems electromagnetic compatibility (EMC). The engineering issues to be addressed in order to achieve system-level EMC are identified herein, with guidance and rationale towards achieving specification conformance. The method for the derivation of typical equipment-level requirements from a space-system-level requirement is illustrated. This document also aids in the selection of tailored requirements for a specific mission (see Annex A).
|
Published |
2022-06 |
Edition : 2 |
Number of pages : 46 |
Technical Committee |
49.140
Space systems and operations
;
33.100.01
Electromagnetic compatibility in general
|
| ISO 14303:2002 |
Space systems — Launch-vehicle-to-spacecraft interfaces |
ISO 14303 specifies the interfaces between a launch vehicle (LV) and the spacecraft (SC) being launched, to provide LV and SC organizations with the necessary format for presenting the required technical data on existing and future interfaces. Its intended purpose is to minimize costs and reduce the risks from errors resulting from miscommunication. It does not limit the ability of LV or SC organizations to specify unique requirements.
|
Published |
2002-10 |
Edition : 1 |
Number of pages : 54 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14619:2003 |
Space systems — Space experiments — General requirements |
ISO 14619:2003 specifies the procedure for preparing and carrying out space experiments and processing the resulting data, and applies to both manned and unmanned space systems, excluding exploratory rockets with associated probes. It may be tailored to the specific needs of different kinds of experiments and their carrier space vehicles.
|
Withdrawn |
2003-10 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14619:2023 |
Space systems — Space experiments — General requirements |
This document addresses experimental add-on components to a space system under development and specifies the procedures for preparing and carrying out space experiments (SEs), and analysis and processing of the findings.
It is applicable to both manned and unmanned space systems. It can be tailored to the specific needs of different kinds of SEs.
|
Published |
2023-01 |
Edition : 2 |
Number of pages : 12 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14620-1:2002 |
Space systems — Safety requirements — Part 1: System safety |
ISO 14620-1:2002 defines the safety programme and the technical safety requirements that are implemented in order to comply with the safety policy as defined in ISO 14300-2. It is intended to protect flight and ground personnel, the launch vehicle, associated payloads, ground support equipment, the general public, public and private property, and the environment from hazards associated with space systems. Launch site operations are described by ISO 14620-2.
The safety policy is applied by implementing a system safety programme, supported by risk assessment, which can be summarized as follows: hazardous characteristics (system and environmental hazards) and functions with potentially hazardous failure effects are identified and progressively evaluated by iteratively performing systematic safety analyses; the potential hazardous consequences associated with the system characteristics and functional failures are subjected to a hazard reduction sequence whereby hazards are eliminated from the system design and operations, hazards are minimized, and hazard controls are applied and verified; the risks that remain after the application of a hazard elimination and reduction process are progressively assessed and subjected to risk assessment, in order to show compliance with safety targets, support design trades, identify and rank risk contributors, support apportionment of project resources for risk reduction, assess risk reduction progress, and support the safety and project decision-making process (e.g. waiver approval, residual risk acceptance); the adequacy of the hazard and risk control measures applied are formally verified in order to support safety validation and risk acceptance; safety compliance is assessed by the project and safety approval obtained from the relevant authorities.
ISO 14620-1:2002 is applicable to all space projects where during any project phase there exists the potential for hazards to personnel or the general public, space flight systems, ground support equipment, facilities, public or private property, or the environment.
The imposition of these requirements on the project suppliers' activities requires that the customer's project product assurance and safety organization also respond to these requirements in a manner which is commensurate with the project's safety criticality.
When viewed from the perspective of a specific programme or project context, the requirements defined in ISO 14620-1:2002 should be tailored to match the genuine requirements of a particular profile and circumstances of a programme or project.
|
Withdrawn |
2002-12 |
Edition : 1 |
Number of pages : 37 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14951-4:1999 |
Space systems — Fluid characteristics — Part 4: Helium |
|
Withdrawn |
1999-09 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14620-1:2018 |
Space systems — Safety requirements — Part 1: System safety |
This document defines the safety programme and the technical safety requirements that are implemented in order to comply with the safety policy as defined in ISO 14300‑2. It is intended to protect flight and ground personnel, the launch vehicle, associated payloads, ground support equipment, the general public, public and private property, and the environment from hazards associated with space systems. Launch site operations are described by ISO 14620‑2 and flight safety systems in ISO 14620‑3.
The safety policy is applied by implementing a system safety programme, supported by risk assessment, which can be summarized as follows.
a) Hazardous characteristics (system and environmental hazards) and functions with potentially hazardous failure effects are identified and progressively evaluated by iteratively performing systematic safety analyses.
b) The potential hazardous consequences associated with the system characteristics and functional failures are subjected to a hazard reduction sequence whereby:
hazards are eliminated from the system design and operations;
hazards are minimized; and
hazard controls are applied and verified.
c) The risks that remain after the application of a hazard elimination and reduction process are progressively assessed and subjected to risk assessment, in order to:
show compliance with safety targets;
support design trades;
identify and rank risk contributors;
support apportionment of project resources for risk reduction;
assess risk reduction progress; and
support the safety and project decision-making process (e.g. waiver approval, residual risk acceptance).
d) The adequacy of the hazard and risk control measures applied are formally verified in order to support safety validation and risk acceptance.
e) Safety compliance is assessed by the project and safety approval obtained from the relevant authorities.
|
Published |
2018-09 |
Edition : 2 |
Number of pages : 36 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14620-2:2000 |
Space systems — Safety requirements — Part 2: Launch site operations |
|
Withdrawn |
2000-11 |
Edition : 1 |
Number of pages : 15 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14620-2:2011 |
Space systems — Safety requirements — Part 2: Launch site operations |
ISO 14620:2011 specifies requirements for the safety liabilities of countries undertaking space activities or allowing operators to perform space activities on or from their territory under outer space treaties adopted by the United Nations. It defines the safety responsibilities for the operators involved in commercial or non-commercial space launch activities. ISO 14620:2011 establishes the overall safety requirements to be observed on a launch site for prelaunch (integration, test, checking, preparation, etc.) and launch operations of a space object. It provides the basic principles to enable any operator to implement its own safety methods, tools, and procedures, to ensure the safety of people and personnel, public and private property, and the environment, in a consistent and uniform manner.
|
Withdrawn |
2011-08 |
Edition : 2 |
Number of pages : 16 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14620-2:2019 |
Space systems — Safety requirements — Part 2: Launch site operations |
This document specifies requirements for the safety liabilities of countries undertaking space activities or allowing operators to perform space activities on or from their territory under outer-space treaties adopted by the United Nations. It defines the safety responsibilities for the operators involved in commercial or non-commercial space launch activities. This document establishes the overall safety requirements to be observed on a launch site for prelaunch (integration, test, checking, preparation, etc.) and launch operations of a space object. It provides the basic principles to enable any operator to implement its own safety methods, tools and procedures to ensure the safety of people and personnel, public and private property, and the environment, in a consistent and uniform manner.
The safety requirements for system safety are defined in ISO 14620-1, and the requirements for the flight safety systems in ISO 14620-3.
|
Published |
2019-12 |
Edition : 3 |
Number of pages : 15 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14620-3:2005 |
Space systems — Safety requirements — Part 3: Flight safety systems |
ISO 14620-3:2005 sets out the minimum requirements for Flight Safety Systems, including flight termination systems (externally controlled system or on-board automatic system), tracking systems, and telemetry data transmitting systems for commercial or non commercial launch activities of orbital or sub-orbital, unmanned space vehicles. The intent is to minimize the risk of injury or damage to persons, property or the environment resulting from the launching of space vehicles.
ISO 14620-3:2005 can be applied by any country, by any international organization, whether intergovernmental or not, and by any agency or operator undertaking the launching of space vehicles.
ISO 14620-3:2005 is intended to be applied by any person, organization, entity, operator or launch authority participating in commercial or non-commercial launch activities of orbital or sub-orbital, unmanned space vehicles unless more restrictive requirements are imposed by the launch site country.
|
Withdrawn |
2005-05 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14620-3:2021 |
Space systems — Safety requirements — Part 3: Flight safety systems |
This document sets out the minimum requirements for flight safety systems (FSSs), including flight termination systems (FTSs, externally controlled systems or on-board automatic systems), tracking systems, and telemetry data transmitting systems (TDTSs) for commercial or non-commercial launch activities of orbital or suborbital, unmanned space vehicles. The intent is to minimize the risk of injury or damage to persons, property or the environment resulting from the launching of space vehicles.
This document can be applied by any country, by any international organization, whether intergovernmental or not, and by any agency or operator undertaking the launching of space vehicles.
This document is intended to be applied by any person, organization, entity, operator or launch authority participating in commercial or non-commercial launch activities of orbital, or suborbital, unmanned space vehicles unless more restrictive requirements are imposed by the launch site country.
|
Published |
2021-08 |
Edition : 2 |
Number of pages : 7 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14621-1:2003 |
Space systems — Electrical, electronic and electromechanical (EEE) parts — Part 1: Parts management |
ISO 14621-1:2003 addresses the preferred program elements recommended for EEE parts. ISO 14621-1:2003 is written in general terms as a baseline for developing and implementing a parts program.
|
Withdrawn |
2003-12 |
Edition : 1 |
Number of pages : 45 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14621-2:2003 |
Space systems — Electrical, electronic and electromechanical (EEE) parts — Part 2: Control programme requirements |
ISO 14621-2:2003 establishes technical guidelines for developing and documenting an electrical, electronic and electromechanical (EEE) parts control program, in order to assure that the parts used in the flight hardware are acceptable and possess adequate functional, radiation and reliability characteristics to meet the system requirements. These guidelines are tailorable to the needs of each individual programme based on the project performance criteria, risk tolerance, budget, mission duration, environment, schedule and other considerations. ISO 14621-2:2003 is applicable to all customers and suppliers furnishing flight hardware and is suitable for reference in proposal instructions.
|
Withdrawn |
2003-07 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14621-2:2019 |
Space systems — Electrical, electronic and electromechanical (EEE) parts — Part 2: Control programme requirements |
This document establishes technical guidelines for developing and documenting an electrical, electronic and electromechanical (EEE) parts control program, in order to assure that the parts used in the flight hardware are acceptable and possess adequate functional, radiation and reliability characteristics to meet the system requirements. The family of EEE parts includes electro-optical parts.
This document identifies a set of management guidelines for dealing with space systems engineering activities and defines the minimum existing processes on the subject.
These guidelines are tailorable to the needs of each individual programme based on the project performance criteria, risk tolerance, budget, mission duration, environment, schedule and other considerations. This document is applicable to all customers and suppliers furnishing flight hardware and is suitable for reference in proposal instructions.
|
Published |
2019-05 |
Edition : 2 |
Number of pages : 7 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14622:2000 |
Space systems — Structural design — Loads and induced environment |
This International Standard defines the principles used to determine loads and the induced environment during the
service life of a space flight vehicle and its components, taking account of the notions of probability, combined
loads, corresponding safety factors and lifecycle.
|
Published |
2000-12 |
Edition : 1 |
Number of pages : 9 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14623:2003 |
Space systems - Pressure vessels and pressurized structures — Design and operation |
ISO 14623:2003, based on general space experience and practice, specifies general and detailed requirements for metallic pressure vessels, composite overwrapped pressure vessels with metallic liners and metallic pressurized structures used in space systems. It is not applicable to pressure components (lines, fittings, valves, hoses, etc.) or to special pressurized hardware (batteries, heat pipes, cryostats and sealed containers).
|
Published |
2003-12 |
Edition : 1 |
Number of pages : 30 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14624-1:2003 |
Space systems — Safety and compatibility of materials — Part 1: Determination of upward flammability of materials |
ISO 14624-1:2003 specifies a method for the determination of the flammability of aerospace materials by upward flame propagation. Specifically, this test determines if a material, when exposed to a standard ignition source, will self-extinguish and not transfer burning debris to adjacent materials which can be ignited by such debris.
|
Published |
2003-06 |
Edition : 1 |
Number of pages : 15 |
Technical Committee |
49.140
Space systems and operations
;
13.220.40
Ignitability and burning behaviour of materials and products
;
49.025.01
Materials for aerospace construction in general
|
| ISO/FDIS 14624-1 |
Space systems — Safety and compatibility of materials — Part 1: Determination of upward flammability of materials |
|
Under development |
|
Edition : 2 |
|
Technical Committee |
49.140
Space systems and operations
;
13.220.40
Ignitability and burning behaviour of materials and products
;
49.025.01
Materials for aerospace construction in general
|
| ISO 14624-2:2003 |
Space systems — Safety and compatibility of materials — Part 2: Determination of flammability of electrical-wire insulation and accessory materials |
ISO 14624-2:2003 specifies two test methods for determining the flammability of electrical-wire insulation and accessory materials by exposure to an external ignition source in a static environment (Test A) and in a gas-flow environment (Test B).
|
Published |
2003-06 |
Edition : 1 |
Number of pages : 19 |
Technical Committee |
49.140
Space systems and operations
;
13.220.40
Ignitability and burning behaviour of materials and products
;
49.025.01
Materials for aerospace construction in general
|
| ISO/FDIS 14624-2 |
Space systems — Safety and compatibility of materials — Part 2: Determination of flammability of electrical-wire insulation and accessory materials |
|
Under development |
|
Edition : 2 |
|
Technical Committee |
49.140
Space systems and operations
;
13.220.40
Ignitability and burning behaviour of materials and products
;
49.025.01
Materials for aerospace construction in general
|
| ISO 14951-4:1999/Cor 1:2000 |
Space systems — Fluid characteristics — Part 4: Helium — Technical Corrigendum 1 |
|
Withdrawn |
2000-06 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14624-3:2005 |
Space systems — Safety and compatibility of materials — Part 3: Determination of offgassed products from materials and assembled articles |
ISO 14624-3:2005 specifies a method for determining the identity and quantity of volatile offgassed products from materials and assembled articles utilized in manned, pressurized spacecraft. This test method is not intended to model or simulate spacecraft atmospheres.
|
Published |
2005-01 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.140
Space systems and operations
;
49.025.01
Materials for aerospace construction in general
|
| ISO/DIS 14624-3 |
Space systems — Safety and compatibility of materials — Part 3: Determination of off-gassed products from materials and assembled articles |
|
Under development |
|
Edition : 2 |
Number of pages : 13 |
Technical Committee |
49.140
Space systems and operations
;
49.025.01
Materials for aerospace construction in general
|
| ISO 14624-4:2003 |
Space systems — Safety and compatibility of materials — Part 4: Determination of upward flammability of materials in pressurized gaseous oxygen or oxygen-enriched environments |
ISO 14624-4:2003 specifies a test method for determining the flammability of aerospace materials in pressurized gaseous oxygen (GOX) and oxygen-enriched environments, at ambient temperature. This method may also be used to provide supplementary information by testing at pressures other than the intended use pressure. The standard pressure range for this test method is from ambient to 69 000 kPa.
|
Published |
2003-06 |
Edition : 1 |
Number of pages : 8 |
Technical Committee |
49.140
Space systems and operations
;
13.220.40
Ignitability and burning behaviour of materials and products
;
49.025.01
Materials for aerospace construction in general
|
| ISO 14624-5:2006 |
Space systems — Safety and compatibility of materials — Part 5: Determination of reactivity of system/component materials with aerospace propellants |
ISO 14624-5:2006 specifies test equipment and techniques used to identify interactions resulting from exposure of a material to an aerospace fluid.
ISO 14624-5:2006 may be used to determine the reactivity of system and component materials with aerospace fluids. It is applicable for determining interactive reactions between propellants and materials used in the design, construction, and operation of propellant storage, transfer, and flight systems. While this procedure is an excellent quick screen test for long-term propellant compatibility, it is semi-qualitative, and (if exposures exceed twelve months) long-term tests need to be used to quantify degradation as a function of time under use conditions.
|
Published |
2006-04 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.140
Space systems and operations
;
49.025.01
Materials for aerospace construction in general
|
| ISO/FDIS 14624-5 |
Space systems — Safety and compatibility of materials — Part 5: Determination of reactivity of system/component materials with aerospace propellants |
|
Under development |
|
Edition : 2 |
Number of pages : 10 |
Technical Committee |
49.140
Space systems and operations
;
49.140
Space systems and operations
;
49.025.01
Materials for aerospace construction in general
;
49.025.01
Materials for aerospace construction in general
|
| ISO 14624-6:2006 |
Space systems — Safety and compatibility of materials — Part 6: Determination of reactivity of processing materials with aerospace fluids |
ISO 14624-6:2006 specifies test equipment and techniques used to identify interactions resulting from exposure of a material to an aerospace fluid.
ISO 14624-6:2006 can be used to determine the reactivity of processing materials with aerospace fluids either through intent or casual exposure. It provides a means to determine the effects of minor amounts of fluids, such as a splash or spill, on materials used in ground support processing operations.
|
Published |
2006-04 |
Edition : 1 |
Number of pages : 12 |
Technical Committee |
49.140
Space systems and operations
;
49.025.01
Materials for aerospace construction in general
|
| ISO 14624-7:2006 |
Space systems — Safety and compatibility of materials — Part 7: Determination of permeability and penetration of materials to aerospace fluids |
ISO 14624-7:2006 specifies test equipment and techniques used to identify interactions resulting from exposure of a material to an aerospace fluid.
ISO 14624-7:2006 can be used to determine the reactivity of materials with aerospace fluids. It provides a means to determine the effects of minor amounts of aerospace fluids, such as in a splash or spill, on materials used in ground support processing operations, and in the selection of personal safety equipment.
|
Published |
2006-04 |
Edition : 1 |
Number of pages : 9 |
Technical Committee |
49.140
Space systems and operations
;
49.025.01
Materials for aerospace construction in general
|
| ISO 14625:1999 |
Space systems — Ground support equipment for use at launch, landing, or retrieval sites— General requirements |
|
Withdrawn |
1999-03 |
Edition : 1 |
Number of pages : 22 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.140
Space systems and operations
|
| ISO 14951-5:1999 |
Space systems — Fluid characteristics — Part 5: Nitrogen tetroxide propellant |
|
Withdrawn |
1999-09 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14625:2007 |
Space systems — Ground support equipment for use at launch, landing or retrieval sites — General requirements |
ISO 14625:2007 specifies the general characteristics, performance, design, test, safety, reliability, maintainability and quality requirements for ground support equipment (GSE) and systems intended for use at launch, landing or retrieval-site installations, or other locations that are the responsibility of the launch, landing and retrieval site. ISO 14625:2007 does not specify how to design GSE, but establishes the minimum requirements to provide simple, robust, safe, reliable, maintainable and cost-effective GSE.
ISO 14625:2007 is applicable to the design of non-flight hardware and software used to support the operations of transporting, receiving, handling, assembly, inspection, test, checkout, service, launch and recovery of space vehicles and payloads at the launch, landing or retrieval sites. As such, the requirements of ISO 14625:2007 are optional for hardware used only at the manufacturing, development or test sites prior to arrival at the launch, landing or retrieval sites. However, if such GSE is temporarily used at a launch, landing or retrieval site, for whatever reason, conformity with all the safety-related requirements of ISO 14625:2007 is a minimum requirement for the GSE.
|
Withdrawn |
2007-11 |
Edition : 2 |
Number of pages : 24 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.140
Space systems and operations
|
| ISO 14625:2023 |
Space systems — Ground support equipment for use at launch, landing or retrieval sites — General requirements |
This document specifies the general characteristics, performance, design, test, checkout, maintenance, safety, reliability, maintainability and quality requirements for ground support equipment (GSE) and systems intended for use at launch, landing or retrieval-site installations, or other locations that are the responsibility of the launch, landing and retrieval site. This document does not specify how to design, checkout and maintain GSE, but establishes the minimum requirements to provide simple, robust, safe, reliable, maintainable and cost-effective GSE.
This document is applicable to the design, checkout and maintenance of non-flight hardware and software used to support the operations of transporting, receiving, handling, assembly, inspection, test, checkout, service, launch and recovery of space vehicles and payloads at the launch, landing or retrieval sites. As such, the requirements of this document are optional for hardware used only at the manufacturing, development or test sites prior to arrival at the launch, landing or retrieval sites. However, if such GSE is dual use equipment to be also at a launch, landing or retrieval site, for whatever reason, all the safety-related requirements of this document apply to the GSE.
|
Published |
2023-01 |
Edition : 3 |
Number of pages : 26 |
Technical Committee |
49.100
Ground service and maintenance equipment
;
49.140
Space systems and operations
|
| ISO 14711:2003 |
Space systems — Unmanned mission operations concepts — Guidelines for defining and assessing concept products |
ISO 14711:2003 gives guidelines for areas to be addressed and defines the products that are to be generated to develop a space systems mission operations concept. ISO 14711:2003 enables the generation of standard space systems mission operations concept products produced either by an industry, a government agency, or by a university.
|
Published |
2003-03 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14721:2003 |
Space data and information transfer systems — Open archival information system — Reference model |
ISO 14721:2003 specifies a reference model for an open archival information
system (OAIS). The purpose of this ISO 14721:2003 is to establish a system for
archiving information, both digitalized and physical, with an organizational
scheme composed of people who accept the responsibility to preserve information
and make it available to a designated community.
This reference model addresses a full range of archival information
preservation functions including ingest, archival storage, data management,
access, and dissemination. It also addresses the migration of digital
information to new media and forms, the data models used to represent the
information, the role of software in information preservation, and the exchange
of digital information among archives. It identifies both internal and external
interfaces to the archive functions, and it identifies a number of high-level
services at these interfaces. It provides various illustrative examples and some
"best practice" recommendations. It defines a minimal set of responsibilities
for an archive to be called an OAIS, and it also defines a maximal archive to
provide a broad set of useful terms and concepts.
The OAIS model described in ISO 14721:2003 may be applicable to any archive.
It is specifically applicable to organizations with the responsibility of making
information available for the long term. This includes organizations with other
responsibilities, such as processing and distribution in response to
programmatic needs.
|
Withdrawn |
2003-03 |
Edition : 1 |
Number of pages : 141 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14721:2012 |
Space data and information transfer systems — Open archival information system (OAIS) — Reference model |
ISO 14721:2012 defines the reference model for an open archival information system (OAIS). An OAIS is an archive, consisting of an organization, which may be part of a larger organization, of people and systems that has accepted the responsibility to preserve information and make it available for a designated community. It meets a set of such responsibilities as defined in this International Standard, and this allows an OAIS archive to be distinguished from other uses of the term "archive". The term "open" in OAIS is used to imply that ISO 14721:2012, as well as future related International Standards, are developed in open forums, and it does not imply that access to the archive is unrestricted.
ISO 14721:2012
provides a framework for the understanding and increased awareness of archival concepts needed for long term digital information preservation and access,
provides the concepts needed by non-archival organizations to be effective participants in the preservation process,
provides a framework, including terminology and concepts, for describing and comparing architectures and operations of existing and future archives,
provides a framework for describing and comparing different Long Term Preservation strategies and techniques,
provides a basis for comparing the data models of digital information preserved by archives and for discussing how data models and the underlying information may change over time,
provides a framework that may be expanded by other efforts to cover long term preservation of information that is not in digital form (e.g. physical media and physical samples),
expands consensus on the elements and processes for long term digital information preservation and access, and promotes a larger market which vendors can support, and
guides the identification and production of OAIS-related standards.
|
Published |
2012-09 |
Edition : 2 |
Number of pages : 126 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14952-1:2003 |
Space systems — Surface cleanliness of fluid systems — Part 1: Vocabulary |
ISO 14952-1:2003 defines the basic terms for use in cleaning processes for equipment and components used in space fluid systems. It is applicable to terms used in the description of processes for the cleaning, analysis and verification of fluid systems used in ground support equipment, launch vehicles and spacecraft.
|
Published |
2003-11 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.140
Space systems and operations
|
| ISO 14952-2:2003 |
Space systems — Surface cleanliness of fluid systems — Part 2: Cleanliness levels |
ISO 14952-2:2003 defines the cleanliness levels used in the cleaning, analysis, and verification procedures for space fluid systems. It establishes a common nomenclature for use in describing cleanliness levels for equipment used in ground support equipment, launch vehicles and spacecraft.
ISO 14952-2:2003 is used to specify the cleanliness level of fluid system components and equipment used in space systems. It is applicable equally to ground support equipment, launch vehicles and spacecraft.
|
Published |
2003-11 |
Edition : 1 |
Number of pages : 6 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.140
Space systems and operations
|
| ISO 14952-3:2003 |
Space systems — Surface cleanliness of fluid systems — Part 3: Analytical procedures for the determination of nonvolatile residues and particulate contamination |
ISO 14952-3:2003 provides sampling and analytical test methods to validate the cleanliness levels of parts and components that have been precision cleaned, and identifies processes that may be used for the verification of cleanliness in ground support equipment, launch vehicles and spacecraft. ISO 14952-3:2003 is used to sample and verify the level of cleanliness of parts and components that have been precision cleaned and applies equally to parts, components and systems in ground support equipment, launch vehicles and spacecraft.
|
Published |
2003-11 |
Edition : 1 |
Number of pages : 15 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.140
Space systems and operations
|
| ISO 14952-4:2003 |
Space systems — Surface cleanliness of fluid systems — Part 4: Rough-cleaning processes |
ISO 14952-4:2003 provides requirements related to rough-cleaning processes used to prepare parts and components for precision cleaning. It identifies precleaning processes that can be used for ground support equipment, launch vehicles and spacecraft.
Rough cleaning removes contaminants such as weld scale, heat-treat scale, corrosion, oxide films, oils, grease, shop soil, fuel and carbon deposits. Rough cleaning is considered a normal shop process and usually does not require special environmental controls, packaging, handling or storage beyond accepted good practice.
ISO 14952-4:2003 is applicable equally to ground support equipment, launch vehicles and spacecraft.
|
Published |
2003-11 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.140
Space systems and operations
|
| ISO 14952-5:2003 |
Space systems — Surface cleanliness of fluid systems — Part 5: Drying processes |
ISO 14952-5:2003 provides guidance related to processes used to dry parts and components that have been subjected to solvent-based or water-based cleaning processes, and identifies drying processes that can be used for equipment that has been cleaned for use in ground support equipment, launch vehicles and spacecraft. Vacuum drying can be used to remove entrapped fluids from intricate parts when normal purging methods have been found to be ineffective.
|
Published |
2003-11 |
Edition : 1 |
Number of pages : 3 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.140
Space systems and operations
|
| ISO 14952-6:2003 |
Space systems — Surface cleanliness of fluid systems — Part 6: Precision-cleaning processes |
ISO 14952-6:2003 specifies precision-cleaning processes for parts, components and systems used in flight-critical fluid applications. It can be used on equipment for ground support equipment, launch vehicles and spacecraft.
ISO 14952-6:2003 identifies precision-cleaning processes and procedures that can be used on parts and components used in fluid systems and is applicable equally to ground support equipment, launch vehicles and spacecraft.
|
Published |
2003-11 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.080
Aerospace fluid systems and components
;
49.140
Space systems and operations
|
| ISO 14953:2000 |
Space systems — Structural design — Determination of loading levels for static qualification testing of launch vehicles |
This International Standard specifies a procedure for determining the loading level of a qualification test of a launch
vehicle structure and takes into account all the minimum allowable strength characteristics necessary for these
structures.
This International Standard establishes the required resistance necessary for all mass-produced items to comply
with product assurance criteria.
|
Published |
2000-05 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/CD 14953 |
Space systems — Structural design — Determination of loading levels for static qualification testing of launch vehicles |
This International Standard specifies a procedure for determining the loading level of a qualification test of a launch
vehicle structure and takes into account all the minimum allowable strength characteristics necessary for these
structures.
This International Standard establishes the required resistance necessary for all mass-produced items to comply
with product assurance criteria.
|
Under development |
|
Edition : 2 |
|
Technical Committee |
49.140
Space systems and operations
|
| ISO 14954:2005 |
Space systems — Dynamic and static analysis — Exchange of mathematical models |
ISO 14954:2005 normalizes the exchange of mathematical models between spacecraft contractors (SCC) and launch service providers (LSP). It identifies standard methods for modelling the dynamic behaviour of both launch vehicles (LV) and spacecraft (SC) particularly when they are coupled prior to launch and during the early moments of the launch phase.
In standard mode, the delivered models represent dynamic and static behaviour at the launcher interface. The requirements provided in ISO 14954:2005 are the minimum necessary for dynamic coupled analysis. They may be not sufficient for stress analysis.
ISO 14954:2005 does not include the validation of spacecraft models.
|
Published |
2005-02 |
Edition : 1 |
Number of pages : 13 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14961:1997 |
Space data and information transfer systems — Parameter value language specification |
|
Withdrawn |
1997-12 |
Edition : 1 |
Number of pages : 50 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14961:2002 |
Space data and information transfer systems — Parameter value language specification |
ISO 14961:2002 specifies the requirements for a parameter value language (PVL) specification for space data and information transfer systems. It establishes a standard keyword value type language for naming and expressing data values and provides an overview and formal syntax specification of the PVL. Two versions of PVL are defined, the basic version (CCSD0006) and an extended character set version (CCSD0008).
The specifications in this ISO 14961:2002 are applicable to all space-related science and engineering data exchanges where a keyword value language is desired.
|
Published |
2002-09 |
Edition : 2 |
Number of pages : 81 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 14962:1997 |
Space data and information transfer systems — ASCII encoded English |
|
Published |
1997-12 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/CD 15104 |
Space systems — Environmental testing for spacecraft thermal control materials |
This international standard intends to establish a guideline for the ground-based environmental tests of thermal control materials (TCMs) used on spacecraft’s surface. This standard describes the test methods of charged particle radiation(s), solar ultraviolet (UV), atomic oxygen (AO) and thermal cycling. Typical TCMs include, but are not limited to, coatings, optical solar reflector (OSR) and metallized plastic films. Other materials, for which similar requirements apply, can refer to this standard. This international standard is devoted to material estimation/evaluation tests and can be tailored according to specific applications.
|
Under development |
|
Edition : 1 |
|
Technical Committee |
49.140
Space systems and operations
|
| ISO 15387:2005 |
Space systems — Single-junction solar cells — Measurements and calibration procedures |
ISO 15387:2005 specifies the requirements for measurement and calibration procedures of single-junction space solar cells only. The main body of ISO 15387:2004 specifies the requirements for Air Mass Zero (AM0) standard calibration. The relative measurement procedures are provided as annexes.
|
Published |
2005-06 |
Edition : 1 |
Number of pages : 83 |
Technical Committee |
27.160
Solar energy engineering
;
49.140
Space systems and operations
|
| ISO 15388:2004 |
Space systems — Contamination and cleanliness control |
ISO 15388:2004 establishes general requirements for contamination and cleanliness control to be applied, at all tiers of supply, to the development of space systems including ground processing facilities, ground support equipment, launch vehicles, spacecraft, payloads, and ground processing and on-orbit operations. It also provides guidelines for the establishment of a contamination and cleanliness control programme.
|
Withdrawn |
2004-09 |
Edition : 1 |
Number of pages : 19 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 15388:2012 |
Space systems — Contamination and cleanliness control |
This International Standard establishes general requirements for contamination and cleanliness control that are applicable, at all tiers of supply, to the development of space systems, including ground processing facilities, ground support equipment, launch vehicles, spacecraft, payloads, and ground processing and on-orbit operations. It also provides guidelines for the establishment of a contamination and cleanliness control programme.
|
Withdrawn |
2012-02 |
Edition : 2 |
Number of pages : 20 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 15388:2022 |
Space systems — Contamination and cleanliness control |
This document establishes general requirements for contamination and cleanliness control that are applicable, at all tiers of supply, to the development of space systems, including ground processing facilities, ground support equipment, launch vehicles, spacecraft, payloads, and ground processing and on-orbit operations. It also provides guidelines for the establishment of a contamination and cleanliness control programme.
|
Published |
2022-10 |
Edition : 3 |
Number of pages : 32 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 15389:2001 |
Space systems — Flight-to-ground umbilicals |
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.
|
Published |
2001-01 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/DIS 15389 |
Space systems — Flight-to-ground umbilicals |
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.
|
Under development |
|
Edition : 2 |
Number of pages : 15 |
Technical Committee |
49.140
Space systems and operations
|