| Name |
Description |
Abstract |
Status |
Publication date |
Edition |
Number of pages |
Technical committee |
ICS |
| ISO 21349 |
Space systems — Project reviews |
ISO 21349:2007 provides process requirements for project reviews as a set of required functions. The requirements and recommendations cover the function inputs, outputs, mechanisms, and controlling conditions. It is intended for use in implementing the review requirements of ISO 14300-1, ISO 14300-2, ISO 15865, and such other space systems and operations standards that require formal reviews.
ISO 21349:2007 specifies the responsibilities of a review board and gives guidance concerning review board composition.
ISO 21349:2007 is applicable to reviews for a project at any level within a larger project, as well as for major milestone reviews at the top level of a major project. It is intended to be used either by an independent developer as a basis for enterprise processes, or as a basis for an agreement between a supplier and a customer.
ISO 21349:2007 also provides normative descriptions of the kinds of reviews that are commonly useful in assuring the success of a space project.
|
Under development |
2023-04 |
Edition : 2 |
|
Technical Committee |
49.140
Space systems and operations
|
| ISO 3102:1981 |
Wheels and castors for non-powered equipment — Off-set for swivel castors |
Does not cover wheels used for furniture and toys. Gives the dimensions (diameter of wheel related to off-set).
|
Withdrawn |
1981-10 |
Edition : 2 |
Number of pages : 1 |
Technical Committee |
53.060
Industrial trucks
|
| ISO 21442:2022 |
Space systems — General requirements for control engineering |
This document deals with control systems developed as part of a space project. It is applicable to all the elements of a space control system, including the space segment, the ground segment and the launch service segment.
This document establishes general principles for all technical activities of space control engineering, including control engineering management, requirements definition, analysis, design, production, verification and validation, operation, maintenance, and disposal. It also provides requirements to progressively refine and manage control system realizations in space systems including multiple control systems.
The requirements of this document can be tailored for each specific space program application.
|
Published |
2022-05 |
Edition : 1 |
Number of pages : 34 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 21459:2006 |
Space data and information transfer systems — Proximity-1 space link protocol — Coding and synchronization sublayer |
Proximity space links are defined to be short-range, bi-directional, fixed or mobile radio links, generally used to communicate among probes, landers, rovers, orbiting constellations, and orbiting relays. These links are characterized by short time delays, moderate (not weak) signals, and short, independent sessions.
ISO 21459:2006 defines the coding and synchronization sublayer of the Proximity-1 space link protocol. It defines the data unit of this sublayer, i.e. the PLTU. It defines the coding and synchronization mechanisms required for cross support. It also specifies the send and receive side functionality of this sublayer. ISO 21459:2006 does not specify
individual implementations or products, implementation of service interfaces within real systems, methods or technologies required to perform the procedures, or management activities required to configure and control the protocol.
|
Withdrawn |
2006-07 |
Edition : 1 |
Number of pages : 25 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 21459:2015 |
Space data and information transfer systems — Proximity-1 space link protocol — Coding and synchronization sublayer |
ISO 21459:2015 defines synchronization and channel coding schemes for Proximity-1 links in terms of:
a) the services provided to the users of this specification;
b) data formats; and
c) the procedures performed to generate and process the data formats.
It does not specify:
a) individual implementations or products;
b) the methods or technologies required to perform the procedures; or
c) the management activities required to configure and control the protocol.
The Coding and Synchronization Sublayer is part of the Data Link Layer. The rest of the Data Link Layer is defined in the separate CCSDS Recommended Standard entitled, Proximity-1 Space Link Protocol?Data Link Layer (reference [3]). The Physical Layer is defined in the separate CCSDS Recommended Standard entitled, Proximity-1 Space Link Protocol?Physical Layer (reference [4]).
|
Published |
2015-08 |
Edition : 2 |
Number of pages : 38 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 21460:2006 |
Space data and information transfer systems — Proximity-1 space link protocol — Physical layer |
Proximity space links are defined to be short-range, bi-directional, fixed or mobile radio links, generally used to communicate among probes, landers, rovers, orbiting constellations, and orbiting relays. These links are characterized by short time delays, moderate (not weak) signals, and short, independent sessions.
ISO 21460:2006 defines the Proximity-1 space link protocol physical layer. The specification for the channel connection process, provision for frequency bands and assignments, hailing channel, polarization, modulation, data rates, and performance requirements are defined in ISO 21460:2006. Currently, the physical layer only defines operations at UHF frequencies for the Mars environment.
ISO 21460:2006 does not specify
individual implementations or products, implementation of service interfaces within real systems, methods or technologies required to perform the procedures, or management activities required to configure and control the protocol.
|
Withdrawn |
2006-07 |
Edition : 1 |
Number of pages : 24 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 21460:2007 |
Space data and information transfer systems — Proximity-1 space link protocol — Physical layer |
ISO 21460:2007 defines the Proximity-1 space link protocol physical layer. It specifies the channel connection process, provision for frequency bands and assignments, hailing channel, polarization, modulation, data rates, and performance requirements. Currently, the physical layer only defines operations at UHF frequencies for the Mars environment. The coding layer is defined in ISO 21459. The data link layer is defined in ISO 22663.
ISO 21460:2007 does not specify
individual implementations or products;
implementation of service interfaces within real systems;
the methods or technologies required to perform the procedures; or
the management activities required to configure and control the protocol.
The scope and field of application are furthermore detailed in subclause 1.3 of the enclosed CCSDS publication.
|
Withdrawn |
2007-10 |
Edition : 2 |
Number of pages : 35 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 21460:2015 |
Space data and information transfer systems — Proximity-1 space link protocol — Physical layer |
ISO 21460:2015 defines the Proximity-1 Space Link Protocol Physical Layer. The specification for the channel connection process, provision for frequency bands and assignments, hailing channel, polarization, modulation, data rates, and performance requirements are defined in this document.
Currently, the Physical Layer only defines operations at UHF frequencies for the Mars environment.
The Data Link Layer is defined in the two separate CCSDS Recommended Standards entitled, Proximity-1 Space Link Protocol?Coding and Synchronization Sublayer (reference [2]), and Proximity-1 Space Link Protocol?Data Link Layer (reference [3]).
ISO 21460:2015 does not specify
a) individual implementations or products;
b) implementation of service interfaces within real systems;
c) the methods or technologies required to perform the procedures; or
d) the management activities required to configure and control the protocol.
|
Published |
2015-08 |
Edition : 3 |
Number of pages : 27 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 21648:2008 |
Space systems — Flywheel module design and testing |
ISO 21648:2008 establishes the design, analysis, material selection and characterization, fabrication, test and inspection of the flywheel module (FM) in a flywheel used for energy storage in space systems. These requirements, when implemented on a flywheel module, will ensure a high level of confidence in achieving safe operation and mission success. With appropriate modifications, ISO 21648:2008 can also be applied to similar devices, such as momentum and reaction wheels and control-moment gyroscopes.
The requirements set forth in ISO 21648:2008 are the minimum requirements for flywheel modules in flywheels used in space flight applications. They are specifically applicable to the parts in the flywheel rotor assembly (FRA), including rim, hub and/or shaft and other associated rotating parts, such as the bearings and the motor generator rotor. The requirements are also relevant to the non-rotating parts, such as module housing, main suspension assembly (magnetic or rolling element bearings, superconductor bearings, etc.), motor stator, caging mechanism and sensors within the module housing, and backup bearings, if applicable. However, control and interface electronics are not covered in ISO 21648:2008.
|
Published |
2008-12 |
Edition : 1 |
Number of pages : 28 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 21886:2019 |
Space systems — Configuration management |
This document defines the contents, methods and requirements of configuration management for space projects, and the responsibilities and authorities of related parties. It can be used together with ISO 14300‑1:2011, Clause 10.
This document is applicable to the configuration management of space projects from the mission analysis phase to the disposal phase.
|
Published |
2019-04 |
Edition : 1 |
Number of pages : 29 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 21961:2003 |
Space data and information transfer systems — Data entity dictionary specification language (DEDSL) — Abstract syntax |
ISO 21961:2003 gives requirements and defines the syntax of a specification language to be used in the creation of a data entity dictionary (DED).
A data entity is a concept that can, or does, take on one or more values. Semantics of a data entity, such as a text definition of its meaning, are defined by attributes. The purpose of ISO 21961:2003 is to define a language for specifying a dictionary which describes semantics for a collection of data entities; it does not define a specific dictionary. A dictionary is understood as a mechanism that is able to organize a set of information in a consistent and easily understandable manner, and it is commonly used by humans to look up the meaning of words used in natural languages. Similarly, a data entity dictionary (DED) is used by humans and systems to look up the definition, and other attributes, of data entities used in the definition and generation of data products.
ISO 21961:2003 defines the abstract definition of the semantic information that is required to be conveyed and presents the specification in a layered manner (attributes, entities, dictionaries). This is done so that the actual technique used to convey the information is independent of the information content and, therefore, the same abstract standard can be used within different formatting environments. This also permits the semantic information to be translated to different representations as may be needed when data are transferred across different domains.
ISO 21961:2003 defines the concepts of name, definition, units, and a small set of other standard attributes so that they may be used consistently in the formation of data entity dictionaries. Several classes of data entities are defined. These classes allow making a distinction between the abstract data entities, the models, and the concrete data entities, the data fields in a data product.
|
Published |
2003-03 |
Edition : 1 |
Number of pages : 101 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 21962:2003 |
Space data and information transfer systems — Data entity dictionary specification language (DEDSL) — PVL syntax |
ISO 21962:2003 specifies the requirements for establishing a parameter value language (PVL) to be used in the creation of a data entity dictionary (DED).
ISO 21962:2003 is intended to be used by implementers of data entity dictionaries, and for example, by data producers to construct dictionaries that describe, in a more formal manner, data entities within their data products; by data users to understand data received from data producers who have used ISO 21962:2003 to construct their dictionaries; by an organization that mandates the attributes used to define each entity description in dictionaries used within that organization; by a particular community, such as Earth observation, space physics, archives, etc., to establish a degree of standardization for the contents of any data dictionary associated with a data product (this would be done by using ISO 21962:2003 to define a community-wide data dictionary); by organizations and communities to exchange the contents of a data dictionary in a standardized manner, i.e. to facilitate interoperability.
|
Published |
2003-03 |
Edition : 1 |
Number of pages : 73 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/TS 21979:2018 |
Space environment (natural and artificial) — Procedure for obtaining worst case and confidence level of fluence using the quasi-dynamic model of earth's radiation belts |
This document, by using a model that reproduces the fluctuations of radiation belts, defines the calculation method (orbit, operation period) of the radiation fluence received by a satellite. The quasi-dynamic model of Earth's radiation belts adopts input parameters (index values) to predict variation. The input parameters are selected from those that are easy to obtain data and have high correlation with the variation in Earth's radiation belts.
NOTE This method is an engineering method used for satellite design and similar purposes.
|
Published |
2018-09 |
Edition : 1 |
Number of pages : 18 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 21980:2020 |
Space systems — Evaluation of radiation effects on Commercial-Off-The-Shelf (COTS) parts for use on low-orbit satellite |
This document outlines the evaluation methods for environmental tests that can be conducted on COTS (Commercial-Off-The-Shelf) spacecraft parts intended for use on LEO satellites. The radiation effects considered consist of total dosage, single event, and displacement damage. In addition, this document describes tests that are useful for satellites operating in LEO.
|
Published |
2020-01 |
Edition : 1 |
Number of pages : 47 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22538-2:2007 |
Space systems — Oxygen safety — Part 2: Selection of metallic materials for oxygen systems and components |
ISO 22538-2:2007 describes a process for the selection of metallic materials for oxygen systems and their components. ISO 22538-2:2007 applies equally to ground support equipment, launch vehicles and spacecraft.
|
Published |
2007-09 |
Edition : 1 |
Number of pages : 15 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22009:2009 |
Space systems — Space environment (natural and artificial) — Model of the earth's magnetospheric magnetic field |
ISO 22009:2009 describes the main magnetospheric large-scale current systems and the magnetic field in the earth's magnetosphere and provides the main requirements for a model of the magnetospheric magnetic field. Ionospheric currents are not considered in ISO 22009:2009. ISO 22009:2009 includes a worked example of the model and establishes the parameters of magnetospheric large-scale current systems that change according to conditions in the space environment. ISO 22009:2009 can be used to develop new models of the magnetospheric magnetic field. Such models are useful in investigating the physical processes in the earth's magnetosphere as well as in calculations associated with developing, testing and estimating the results of exploitation of spacecrafts and other equipment operating in the space environment.
The main goals of standardizing the concepts of the earth's magnetospheric magnetic field are to provide an unambiguous presentation of the magnetic field in the earth's magnetosphere; compatibility for the results of the interpretation and analysis of space experiments; less labour-intensive calculations of the magnetic field of magnetospheric currents in space at geocentric distances of 1,0 to 6,6 earth radii, RE; and the most reliable calculations of all elements of the geomagnetic field in the space environment.
The magnetic field model presented in ISO 22009:2009 can be used to predict the radiation conditions in space, including the periods of intense magnetic disturbances (magnetic storms), when developing systems of spacecraft magnetic orientation and when forecasting the influence of magnetic disturbances on transcontinental piping and power transmission lines.
|
Withdrawn |
2009-12 |
Edition : 1 |
Number of pages : 15 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22009:2023 |
Space environment (natural and artificial) — Model of the Earth's magnetospheric magnetic field |
This document describes the main magnetospheric large-scale current systems and the magnetic field in the Earth's magnetosphere and provides the main requirements to the model of the magnetospheric magnetic field. Ionospheric currents are not considered in this document. The document also provides a working example of the model and establishes the parameters of magnetospheric large-scale current systems which are changing in accordance with conditions in the space environment. The document can be used to develop the new models of magnetospheric magnetic field. Such models are useful in investigating physical processes in the Earth's magnetosphere as well as in calculations, developing, testing and estimating the results of exploitation of spacecrafts and other equipment operating in the space environment.
|
Published |
2023-01 |
Edition : 2 |
Number of pages : 17 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22010:2007 |
Space systems — Mass properties control |
ISO 22010:2007 describes a process for managing, controlling and monitoring the mass properties of space systems. The relationship between this management plan and the performance parameters for mass properties to be met throughout the mission is described. Ground handling, dynamics analysis and test set-ups that rely on accurate mass properties inputs are identified. ISO 22010:2007 covers all programme phases from pre-proposal through to end of life.
|
Withdrawn |
2007-12 |
Edition : 1 |
Number of pages : 13 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22010:2022 |
Space systems — Mass properties control |
This document describes a process for managing, controlling and monitoring the mass properties of space systems. The relationship between this management plan and the performance parameters for mass properties to be met throughout the mission is described. Ground handling, dynamics analysis and test set-ups that rely on accurate mass properties inputs are identified. This document covers all programme phases from pre-proposal through to end of life.
|
Published |
2022-11 |
Edition : 2 |
Number of pages : 12 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22108:2008 |
Space systems — Non-flight items in flight hardware — Identification and control |
ISO 22108:2008 describes the identification of critical non-flight items in space flight hardware and the procedure to account for their complete removal prior to flight. ISO 22108:2008 is used in context with project-specific quality requirements and procedures related to flight hardware and related activities prior to launch and at the launch site. Verification of removal of critical non-flight items is described in ISO 22108:2008.
Removal of other non-flight items is outside the scope of ISO 22108:2008 and is verified by relevant inspection procedures.
|
Published |
2008-12 |
Edition : 1 |
Number of pages : 9 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22137:2020 |
Space systems — Program management — Test reviews |
This document defines procedures, contents and requirements for test reviews which are composed of the Test Readiness Review (TRR), Post Test Review (PTR) and Test Review Board (TRB).
This document is applicable to tests of space systems and space products, including environment tests and functional and performance tests, especially for system level tests and complicated tests.
|
Published |
2020-02 |
Edition : 1 |
Number of pages : 20 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/TS 22295:2021 |
Space environment (natural and artificial) — Modelling of space environment impact on nanostructured materials — General principles |
The document considers peculiarities of the space environment impact on a special kind of materials: nanostructured materials (i.e. materials with structured objects which size in at least one dimension lies within 1 nm to 100 nm) and specifies the methods of mathematical simulation of such processes. It emphasizes the necessity of applying multiscale simulation approach and does not include any special details concerning concrete materials, elements of spacecraft construction and equipment, etc.
This document provides the general description of the methodology of applying computer simulation methods which relate to different space and time scales to modelling processes occurring in nanostructured materials under the space environment impact.
The document can be applied as a reference document in spacecraft designing, forecasting the spacecraft lifetime, conducting ground-based tests, and analysing changes of material properties during operation.
|
Published |
2021-05 |
Edition : 1 |
Number of pages : 29 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 3184:1974 |
Reach and straddle fork lift trucks — Stability tests |
|
Withdrawn |
1974-12 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
53.060
Industrial trucks
|
| ISO 22538-6:2010 |
Space systems — Oxygen safety — Part 6: Facility planning and implementation |
ISO 22538-6:2010 describes a process to ensure the protection and safety of personnel and equipment associated with oxygen systems and components. ISO 22538-6:2010 applies to ground support equipment, launch vehicles and spacecraft.
|
Published |
2010-08 |
Edition : 1 |
Number of pages : 19 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/TS 22591:2021 |
Space systems — Space-based services for a high accuracy positioning system with safety requirements |
This document provides requirements and recommendation for space-based systems that, using satellite radionavigation services, provide high accuracy positioning of rovers. It is particularly intended for rovers whose operation requires meeting specific safety requirements, including in situations of low visibility. This document also provides methods to verify the system requirements, as well as complementary information on particular applications (Annex A), mobile mapping systems (Annex B) and augmented positioning (Annexes C and D).
|
Published |
2021-07 |
Edition : 1 |
Number of pages : 21 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/TR 22639:2021 |
Space systems — Design guidelines for multi-geo spacecraft collocation |
This document addresses the design process of a collocation and the basic contents of collocation design process which include considerations, initial collocation strategy design, simulation evaluation of collocation strategy, optimal collocation strategy selection and collocation agreement.
This document gives guidelines for multi-geo spacecraft collocation, and it applies in particular to multi-geo constellation.
|
Published |
2021-07 |
Edition : 1 |
Number of pages : 21 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22641:2005 |
Space data and information transfer systems — TM (telemetry) synchronization and channel coding |
ISO 22641:2005 specifies synchronization and channel coding schemes used in conjunction with the telemetry (TM) space data link protocol as defined by ISO 22645 or the advanced orbiting systems (AOS) space data link protocol defined by ISO 22666. These schemes are to be used over space-to-ground or space-to-space communications links by space missions.
|
Withdrawn |
2005-07 |
Edition : 1 |
Number of pages : 80 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22641:2012 |
Space data and information transfer systems — TM (telemetry) synchronization and channel coding |
ISO 22641:2012 specifies synchronization and channel coding schemes for use with the TM Space Data Link Protocol (according to ISO 22645:2005) or the AOS Space Data Link Protocol (according to ISO 22666:2007), which are intended to be used over space-to-ground or space-to-space communications links by space missions.
ISO 22641:2012 defines synchronization and channel coding schemes in terms of
the services provided to the users of this specification,
data formats, and
the procedures performed to generate and process the data formats.
ISO 22641:2012 does not specify
individual implementations or products,
the methods or technologies required to perform the procedures, or
the management activities required to configure and control the system.
|
Published |
2012-07 |
Edition : 2 |
Number of pages : 106 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22642:2005 |
Space data and information transfer systems — TC (telecommand) synchronization and channel coding |
ISO 22642:2005 defines synchronization and channel coding schemes used with the telecommand (TC) space data link protocol as defined in ISO 22664. These schemes are to be used over ground-to-space or space-to-space communications links by space missions.
|
Withdrawn |
2005-07 |
Edition : 1 |
Number of pages : 50 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22642:2005/Cor 1:2007 |
Space data and information transfer systems — TC (telecommand) synchronization and channel coding — Technical Corrigendum 1 |
|
Withdrawn |
2007-10 |
Edition : 1 |
Number of pages : 4 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22642:2015 |
Space data and information transfer systems — TC synchronization and channel coding |
ISO 22642:2015 defines synchronization and channel coding schemes in terms of:
a) the services provided to the users of this specification;
b) data formats; and
c) the procedures performed to generate and process the data formats.
It does not specify:
a) individual implementations or products;
b) the methods or technologies required to perform the procedures; or
c) the management activities required to configure and control the system.
|
Published |
2015-11 |
Edition : 2 |
Number of pages : 41 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22643:2003 |
Space data and information transfer systems — Data entity dictionary specification language (DEDSL) — XML/DTD Syntax |
ISO 22643:2003 specifies the requirements for an extensible-markup-language (XML)/document-type-declaration (DTD) syntax for a data entity dictionary specification language (DEDSL).
|
Published |
2003-03 |
Edition : 1 |
Number of pages : 99 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 24917:2020 |
Space systems — General test requirements for launch vehicles |
This document establishes general test requirements for launch vehicles equipped with liquid-propellant engines, launched from stationary ground-, sea- and air-based launchers, in all phases of their development.
|
Published |
2020-07 |
Edition : 2 |
Number of pages : 37 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22644:2006 |
Space data and information transfer systems — Orbit data messages |
ISO 22644:2006 specifies two standard message formats for use in transferring spacecraft orbit information between space Agencies: the Orbit Parameter Message (OPM) and the Orbit Ephemeris Message (OEM). Such exchanges are used for
pre-flight planning for tracking or navigation support;scheduling tracking support;carrying out tracking operations (sometimes called metric predicts);performing orbit comparisons;carrying out navigation operations such as orbit propagation.
ISO 22644:2006 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 |
2006-05 |
Edition : 1 |
Number of pages : 50 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22645:2005 |
Space data and information transfer systems — TM (telemetry) space data link protocol |
ISO 22645:2005 specifies the telemetry (TM) space data link protocol, a data link layer protocol as defined in ISO/IEC 7498-1, and is be used over space-to-ground or space-to-space communications links by space missions.
|
Withdrawn |
2005-07 |
Edition : 1 |
Number of pages : 96 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22645:2005/Amd 1:2015 |
Space data and information transfer systems — TM (telemetry) space data link protocol — Amendment 1 |
|
Withdrawn |
2015-07 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22645:2016 |
Space data and information transfer systems — TM (telemetry) space data link protocol |
ISO 22645:2016 defines the TM Space Data Link Protocol in terms of:
a) the services provided to the users of this protocol;
b) the protocol data units employed by the protocol; and
c) the procedures performed by the protocol.
It does not specify:
a) individual implementations or products;
b) the implementation of service interfaces within real systems;
c) the methods or technologies required to perform the procedures; or
d) the management activities required to configure and control the protocol.
|
Published |
2016-11 |
Edition : 2 |
Number of pages : 100 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22646:2005 |
Space data and information transfer systems — Space packet protocol |
ISO 22646:2005 specifies the space packet protocol for transferring space application data over a network involving a ground-to-space or space-to-space communications link.
|
Published |
2005-07 |
Edition : 1 |
Number of pages : 55 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22646:2005/Amd 1:2015 |
Space data and information transfer systems — Space packet protocol — Amendment 1 |
|
Published |
2015-07 |
Edition : 1 |
Number of pages : 1 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22647:2006 |
Space data and information transfer systems — Space link identifiers |
ISO 22647:2006 specifies the identifiers currently used by the space link protocols and shows how these identifiers are managed at the level of the Consultative Committee for Space Data Systems (CCSDS). It does not specify how these identifiers are managed in individual data systems of space projects.
|
Withdrawn |
2006-02 |
Edition : 1 |
Number of pages : 35 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22647:2010 |
Space data and information transfer systems — Space link identifiers |
ISO 22647:2010 specifies the identifiers currently used by the space link protocols and shows how these identifiers are managed at the CCSDS level. It does not specify how these identifiers are managed in individual data systems of space projects.
|
Withdrawn |
2010-09 |
Edition : 2 |
Number of pages : 22 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22663:2006 |
Space data and information transfer systems — Proximity-1 space link protocol — Data link layer |
ISO 22663:2006 defines the data link layer (framing, media access, data services and input-output sublayers) of a Proximity-1 space link protocol. The specifications for the protocol data units, framing, media access control, expedited and sequenced controlled data transfer, timing service, i/o control as well as the procedures for establishing and terminating a session between a caller and responder are defined in ISO 22663:2006.
ISO 22663:2006 does not specify
individual implementations or products, implementation of service interfaces within real systems, methods or technologies required to perform the procedures, or management activities required to configure and control the protocol.
|
Withdrawn |
2006-04 |
Edition : 1 |
Number of pages : 132 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22666:2016 |
Space data and information transfer systems — AOS (advanced orbiting systems) space data link protocol |
ISO 22666:2016 defines the AOS Space Data Link Protocol in terms of:
a) the services provided to the users of this protocol;
b) the protocol data units employed by the protocol; and
c) the procedures performed by the protocol.
It does not specify:
a) individual implementations or products;
b) the implementation of service interfaces within real systems;
c) the methods or technologies required to perform the procedures; or
d) the management activities required to configure and control the protocol.
|
Published |
2016-11 |
Edition : 3 |
Number of pages : 96 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22663:2007 |
Space data and information transfer systems — Proximity-1 space link protocol — Data link layer |
ISO 22663:2007 defines the Proximity-1 space link protocol data link layer (framing, media access, data services, and input-output sublayers). It specifies the protocol data units, framing, media access control, expedited and sequenced controlled data transfer, timing service, i/o control, as well as the procedures for establishing and terminating a session between a caller and responder. The coding and synchronization sublayer is defined in ISO 21459. The physical layer is defined in ISO 21460.
ISO 22663:2007 does not specify
individual implementations or products;
implementation of service interfaces within real systems;
the methods or technologies required to perform the procedures; or
the management activities required to configure and control the protocol.
The scope and field of application are furthermore detailed in subclause 1.3 of the enclosed CCSDS publication.
|
Withdrawn |
2007-10 |
Edition : 2 |
Number of pages : 139 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22663:2015 |
Space data and information transfer systems — Proximity-1 space link protocol — Data link layer |
ISO 22663:2015 defines the Data Link Layer (Framing, Medium Access Control, Data Services, and Input/Output [I/O] Sublayers). The specifications for the protocol data units, framing, media access control, expedited and sequenced-controlled data transfer, timing service, I/O control, and the procedures for establishing and terminating a session between a caller and responder are defined in this document. The Coding and Synchronization Sublayer is defined in the separate CCSDS Recommended Standard entitled, Proximity-1 Space Link Protocol?Coding and Synchronization Sublayer (reference [5]). The Physical Layer is defined in the separate CCSDS Recommended Standard entitled, Proximity-1 Space Link Protocol?Physical Layer (reference [6]).
ISO 22663:2015 does not specify a) individual implementations or products, b) implementation of service interfaces within real systems, c) the methods or technologies required to perform the procedures, or d) the management activities required to configure and control the protocol.
|
Published |
2015-08 |
Edition : 3 |
Number of pages : 151 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22664:2005 |
Space data and information transfer systems — TC (telecommand) space data link protocol |
ISO 22664:2005 specifies the telecommand (TC) space data link protocol, a data link layer protocol as defined in ISO/IEC 7498-1, that is to be used over ground-to-space or space-to-space communications links by space missions.
|
Withdrawn |
2005-07 |
Edition : 1 |
Number of pages : 110 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22664:2013 |
Space data and information transfer systems — TC (telecommand) space data link protocol |
ISO 22664:2013 specifies the telecommand (TC) space data link protocol. This protocol is a data link layer protocol (as defined in ISO/IEC 7498-1) intended for use over ground-to-space or space-to-space communications links by space missions.
ISO 22664:2013 defines the TC space data link protocol in terms of
the services provided to the users of this protocol,
the protocol data units employed by the protocol, and
the procedures performed by the protocol.
It does not specify
individual implementations or products,
the implementation of service interfaces within real systems,
the methods or technologies required to perform the procedures, or
the management activities required to configure and control the protocol.
|
Withdrawn |
2013-06 |
Edition : 2 |
Number of pages : 106 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22664:2013/Amd 1:2015 |
Space data and information transfer systems — TC (telecommand) space data link protocol — Amendment 1 |
|
Withdrawn |
2015-07 |
Edition : 2 |
Number of pages : 1 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22664:2016 |
Space data and information transfer systems — TC (telecommand) space data link protocol |
ISO 22664:2016 defines the TC Space Data Link Protocol in terms of:
a) the services provided to the users of this protocol;
b) the protocol data units employed by the protocol; and
c) the procedures performed by the protocol.
It does not specify:
a) individual implementations or products;
b) the implementation of service interfaces within real systems;
c) the methods or technologies required to perform the procedures; or
d) the management activities required to configure and control the protocol.
|
Published |
2016-11 |
Edition : 3 |
Number of pages : 116 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22666:2005 |
Space data and information transfer systems — AOS (advanced orbiting systems) space data link protocol |
ISO 22666:2005 specifies the advanced orbiting systems (AOS) space data link protocol, a data link layer protocol as defined in ISO/IEC 7498-1, that is to be used over space-to-ground, ground-to-space, or space-to-space communications links by space missions.
|
Withdrawn |
2005-07 |
Edition : 1 |
Number of pages : 97 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22666:2007 |
Space data and information transfer systems — AOS (advanced orbiting systems) space data link protocol |
ISO 22666:2007 specifies the advanced orbiting systems (AOS) space data link protocol, a data link layer protocol as defined in ISO/IEC 7498-1, that is to be used over space-to-ground, ground-to-space, or space-to-space communications links by space missions.
|
Withdrawn |
2007-09 |
Edition : 2 |
Number of pages : 95 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22666:2007/Amd 1:2015 |
Space data and information transfer systems — AOS (advanced orbiting systems) space data link protocol — Amendment 1 |
|
Withdrawn |
2015-07 |
Edition : 2 |
Number of pages : 1 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22667:2005 |
Space data and information transfer systems — Communication operations Procedure-1 |
ISO 22667:2005 specifies the communications operation Procedure-1 (COP-1). This procedure is used in conjunction with the telecommand (TC) space data link protocol, as defined by ISO 22664, to enable the delivery of service data units to the receiving end of the layer above, correct and without omission or duplication, and in the same sequential order in which they were received from the layer above at the sending end.
|
Withdrawn |
2005-07 |
Edition : 1 |
Number of pages : 88 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22667:2013 |
Space data and information transfer systems — Communications operation procedure-1 |
ISO 22667:2013 specifies the communications operation procedure-1 (COP-1). This procedure is used with the telecommand (TC) space data link protocol (as defined in ISO 22664:2013) to enable the delivery of service data units to the receiving end of the layer above, correct and without omission or duplication, and in the same sequential order in which they were received from the layer above at the sending end.
ISO 22667:2013 defines the COP-1 in terms of
the interfaces with the other procedures,
the internal variables used by the protocol entity,
the actions performed by the protocol entity, and
the state transitions of the protocol entity.
It does not specify
individual implementations or products,
the implementation of service interfaces within real systems,
the methods or technologies required to perform the procedures, or
the management activities required to configure and control the protocol.
|
Published |
2013-06 |
Edition : 2 |
Number of pages : 82 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22669:2003 |
Space data and information transfer systems — Space link extension (SLE) — Return-all-frames service |
ISO 22669:2003 specifies a return-all-frames (RAF) service for a space link extension (SLE) service. The RAF service is an SLE transfer service that delivers all telemetry frames to a mission user from one space link physical channel.
ISO 22669:2003 defines, in an abstract manner, the RAF service in terms of the operations necessary to provide the service; the parameter data associated with each operation; the behaviors that result from the invocation of each operation; and the relationship between, and the valid sequence of, the operations and resulting behaviors.
|
Withdrawn |
2003-12 |
Edition : 1 |
Number of pages : 135 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22669:2007 |
Space data and information transfer systems — Space link extension (SLE) — Return-all-frames service |
ISO 22669:2007 defines the space link extension (SLE) return-all-frames (RAF) service in conformance with ISO 15396:1998. The RAF service is an SLE transfer service that delivers to a mission user all telemetry frames from one space link physical channel.
ISO 22669:2007 defines, in an abstract manner, the RAF service in terms of
the operations necessary to provide the service;the parameter data associated with each operation;the behaviors that result from the invocation of each operation; andthe relationship between, and the valid sequence of, the operations and resulting behaviors.
It does not specify
individual implementations or products;the implementation of entities or interfaces within real systems;the methods or technologies required to acquire telemetry frames from signals received from a spacecraft;the methods or technologies required to provide a suitable environment for communications; orthe management activities required to schedule, configure, and control the RAF service.
|
Withdrawn |
2007-02 |
Edition : 2 |
Number of pages : 143 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22669:2013 |
Space data and information transfer systems — Space link extension (SLE) — Return-all-frames service |
ISO 22669:2013 defines the space link extension (SLE) return-all-frames (RAF) service in conformance with the SLE reference model (ISO 15396:2007). The RAF service is an SLE transfer service that delivers to a mission user all telemetry frames from one space link physical channel.
ISO 22669:2013 defines the RAF service in terms of
the operations necessary to provide the service,
the parameter data associated with each operation,
the behaviors that result from the invocation of each operation, and
the relationship between, and the valid sequence of, the operations and resulting behaviors.
It does not specify
individual implementations or products,
the implementation of entities or interfaces within real systems,
the methods or technologies required to acquire telemetry frames from signals received from a spacecraft,
the methods or technologies required to provide a suitable environment for communications, or
the management activities required to schedule, configure, and control the RAF service.
|
Withdrawn |
2013-06 |
Edition : 3 |
Number of pages : 140 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22669:2021 |
Space data and information transfer systems — Space link extension (SLE) — Return-all-frames service specification |
This document defines, in an abstract manner, the RAF service in terms of:
the operations necessary to provide the service;
the parameter data associated with each operation;
the behaviors that result from the invocation of each operation; and
the relationship between, and the valid sequence of, the operations and resulting behaviors.
It does not specify:
individual implementations or products;
the implementation of entities or interfaces within real systems;
the methods or technologies required to acquire telemetry frames from signals received from a spacecraft;
the methods or technologies required to provide a suitable environment for communications; or
the management activities required to schedule, configure, and control the RAF service.
|
Published |
2021-06 |
Edition : 4 |
Number of pages : 136 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 6044:1985 |
Shipbuilding and marine structures — Derrick boom heel fittings — Main dimensions |
Lays down the main dimensions for interchangeability and the materials for forks and associated bolts or pins for derrick boom heel fittings.
|
Published |
1985-12 |
Edition : 1 |
Number of pages : 2 |
Technical Committee |
47.020.40
Lifting and cargo handling equipment
|
| ISO 22670:2006 |
Space data and information transfer systems — Space link extension (SLE) — Return-channel-frames service |
ISO 22670:2006 specifies a return-channel-frames (RCF) service for a space link extension (SLE). The RCF service is an SLE transfer service that delivers to a mission user all telemetry frames from one master channel or one virtual channel.
It defines, in an abstract manner, the RCF service in terms of
the operations necessary to provide the service;the parameter data associated with each operation;the behaviours that result from the invocation of each operation; the relationship between, and the valid sequence of, the operations and resulting behaviours.
|
Withdrawn |
2006-04 |
Edition : 1 |
Number of pages : 145 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22670:2013 |
Space data and information transfer systems — Space link extension (SLE) — Return-channel-frames service |
ISO 22670:2013 defines the space link extension (SLE) return-channel-frames (RCF) service in accordance with the SLE Reference Model (ISO 15396:2007). The RCF service is an SLE transfer service that delivers to a mission user all telemetry frames from one master channel or one virtual channel.
ISO 22670:2013 defines the RCF service in terms of
the operations necessary to provide the service,
the parameter data associated with each operation,
the behaviors that result from the invocation of each operation, and
the relationship between, and the valid sequence of, the operations and resulting behaviors.
It does not specify
individual implementations or products,
the implementation of entities or interfaces within real systems,
the methods or technologies required to acquire telemetry frames from signals received from a spacecraft,
the methods or technologies required to provide a suitable environment for communications, or
the management activities required to schedule, configure, and control the RCF service.
|
Withdrawn |
2013-06 |
Edition : 2 |
Number of pages : 144 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22670:2021 |
Space data and information transfer systems — Space link extension (SLE) — Return-channel-frames service specification |
The purpose of this document is to define the Space Link Extension (SLE) Return Channel Frames (RCF) service in conformance with the SLE Reference Model (reference [1]). The RCF service is an SLE transfer service that delivers to a mission user all telemetry frames from one master channel or one virtual channel.
This document defines, in an abstract manner, the RCF service in terms of:
the operations necessary to provide the service;
the parameter data associated with each operation;
the behaviors that result from the invocation of each operation; and
the relationship between, and the valid sequence of, the operations and resulting behaviors.
It does not specify:
individual implementations or products;
the implementation of entities or interfaces within real systems;
the methods or technologies required to acquire telemetry frames from signals received from a spacecraft;
the methods or technologies required to provide a suitable environment for communications; or
the management activities required to schedule, configure, and control the RCF service.
NOTE – Reference [1] defines the Return Master Channel Frames (Rtn MC Frames) service and the Return Virtual Channel Frames (Rtn VC Frames) service as two distinct services. Subsequent study has indicated that it is preferable to define one service that provides the functionality of both. The RCF service defined here does just that. It is anticipated that a future issue of reference [1] will take the same approach, deleting the Rtn MC Frames and Rtn VC Frames services and replacing them with the RCF service.
|
Published |
2021-06 |
Edition : 3 |
Number of pages : 141 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22671:2005 |
Space data and information transfer systems — Space link extension (SLE) — Forward command link transmission unit (CLTU) |
ISO 22671:2005 specifies the forward command link transmission unit (CLTU) that may be provided by a space link extension (SLE) system for inter-agency cross support. The CLTU service is an SLE transfer service that enables a mission to send CLTUs to a spacecraft.
|
Withdrawn |
2005-06 |
Edition : 1 |
Number of pages : 141 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22671:2007 |
Space data and information transfer systems — Space link extension (SLE) — Forward communications link transmission unit (CLTU) service |
ISO 22671:2007 defines the communications link transmission unit (CLTU) service in conformance with the transfer services specified in ISO 15396:1998. The forward CLTU service is a space link extension (SLE) transfer service that enables a mission to send communications link transmission units (CLTUs) to a spacecraft.
ISO 22671:2007 defines, in an abstract manner, the forward CLTU service in terms of
the operations necessary to provide the transfer service;the parameter data associated with each operation;the behaviors that result from the invocation of each operation; andthe relationship between, and the valid sequence of, the operations and resulting behaviors.
It does not specify
individual implementations or products;the implementation of entities or interfaces within real systems;the methods or technologies required to radiate data to a spacecraft and to acquire telemetry frames from the signals received from that spacecraft for extraction of the Operational Control Field;the methods or technologies required for communications; orthe management activities necessary to schedule, configure, and control the forward CLTU service.
|
Withdrawn |
2007-02 |
Edition : 2 |
Number of pages : 149 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22671:2011 |
Space data and information transfer systems — Space link extension (SLE) — Forward communications link transmission unit (CLTU) service |
ISO 22671:2011 defines the Communications Link Transmission Unit (CLTU) service in conformance with the transfer services specified in CCSDS 910.4-B-2 (equivalent to ISO 15396). The Forward CLTU service is a Space Link Extension (SLE) transfer service that enables a mission to send Communications Link Transmission Units (CLTUs) to a spacecraft.
ISO 22671:2011 defines, in an abstract manner, the Forward CLTU service in terms of the operations necessary to provide the transfer service, the parameter data associated with each operation, the behaviors that result from the invocation of each operation, and the relationship between, and the valid sequence of, the operations and resulting behaviors.
ISO 22671:2011 does not specify individual implementations or products, the implementation of entities or interfaces within real systems, the methods or technologies required to radiate data to a spacecraft and to acquire telemetry frames from the signals received from that spacecraft for extraction of the Operational Control Field, the methods or technologies required for communications, or the management activities necessary to schedule, configure, and control the Forward CLTU service.
|
Withdrawn |
2011-11 |
Edition : 3 |
Number of pages : 159 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22671:2021 |
Space data and information transfer systems — Space link extension (SLE) — Forward communications link transmission unit (CLTU) service specification |
This document defines the Communications Link Transmission Unit (CLTU) service in conformance with the transfer services specified in reference [1], Cross Support Reference Model—Part 1: SLE Services. The Forward CLTU service is a Space Link Extension (SLE) transfer service that enables a mission to send Communications Link Transmission Units (CLTUs) to a spacecraft.
This document defines, in an abstract manner, the Forward CLTU service in terms of:
the operations necessary to provide the transfer service;
the parameter data associated with each operation;
the behaviors that result from the invocation of each operation; and
the relationship between, and the valid sequence of, the operations and resulting behaviors.
It does not specify:
individual implementations or products;
the implementation of entities or interfaces within real systems;
the methods or technologies required to radiate data to a spacecraft and to acquire telemetry frames from the signals received from that spacecraft for extraction of the Operational Control Field;
the methods or technologies required for communications; or
the management activities necessary to schedule, configure, and control the Forward CLTU service.
|
Published |
2021-06 |
Edition : 4 |
Number of pages : 143 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22672:2006 |
Space data and information transfer systems — Space link extension (SLE) — Forward space packet service |
The Forward Space Packet (FSP) service is a Space Link Extension (SLE) transfer service that enables a mission to send Space Packets to a spacecraft in sequence-controlled or expedited mode. ISO 22672:2006 defines, in an abstract manner, the FSP service in terms of
the operations necessary to provide the transfer service;the parameter data associated with each operation;the behaviours that result from the invocation of each operation;the relationship between, and the valid sequence of, the operations and resulting behaviours.
It does not specify
individual implementations or products;the implementation of entities or interfaces within real systems;the methods or technologies required to radiate Space Packets to a spacecraft and to acquire telemetry frames from the signals received from that spacecraft for extraction of the Operational Control Field;the methods or technologies required for communications;the management activities necessary to schedule, configure, and control the FSP service.
|
Withdrawn |
2006-06 |
Edition : 1 |
Number of pages : 194 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22672:2011 |
Space data and information transfer systems — Space link extension (SLE) — Forward space packet service specification |
ISO 22672:2011 defines the Forward Space Packet (FSP) service in conformance with the transfer services specified in CCSDS 910.4-B-2 (equivalent to ISO 15396). The FSP service is a Space Link Extension (SLE) transfer service that enables a mission to send Space Packets to a spacecraft in sequence-controlled or expedited mode.
ISO 22672:2011 defines, in an abstract manner, the FSP service in terms of the operations necessary to provide the transfer service, the parameter data associated with each operation, the behaviors that result from the invocation of each operation, and the relationship between, and the valid sequence of, the operations and resulting behaviors.
ISO 22672:2011 does not specify individual implementations or products, the implementation of entities or interfaces within real systems, the methods or technologies required to radiate Space Packets to a spacecraft and to acquire telemetry frames from the signals received from that spacecraft for extraction of the Operational Control Field, the methods or technologies required for communications, or the management activities necessary to schedule, configure, and control the FSP service.
|
Withdrawn |
2011-11 |
Edition : 2 |
Number of pages : 209 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22672:2021 |
Space data and information transfer systems — Space link extension (SLE) — Forward space packet service specification |
This document defines the Forward Space Packet (FSP) service in conformance with the transfer services specified in reference [1], Cross Support Reference Model―Part 1: SLE Services. The FSP service is a Space Link Extension (SLE) transfer service that enables a mission to send Space Packets to a spacecraft in sequence-controlled or expedited mode.
This document defines, in an abstract manner, the FSP service in terms of:
the operations necessary to provide the transfer service;
the parameter data associated with each operation;
the behaviors that result from the invocation of each operation; and
the relationship between, and the valid sequence of, the operations and resulting behaviors.
It does not specify:
individual implementations or products;
the implementation of entities or interfaces within real systems;
the methods or technologies required to radiate Space Packets to a spacecraft and to acquire telemetry frames from the signals received from that spacecraft for extraction of the Operational Control Field;
the methods or technologies required for communications; or
the management activities necessary to schedule, configure, and control the FSP service.
NOTE – While the FSP service as described in reference [1] is conceived to handle a variety of packet data structures, this version of the FSP Recommended Standard is restricted to the handling of Space Packets as defined in reference [6].
This version of the FSP Recommended Standard is specific to the transfer of Space Packets to be transmitted via the Telecommand protocol stack as defined in references [3], [4], and [5]. The Cross Support Reference Model (reference [1]) specifies that the FSP service may also be used in conjunction with the Advanced Orbiting System protocol stack, but that mode of operation is outside the scope of this version of the Recommended Standard.
The FSP service is provided in the online delivery mode, as defined in reference [1]. The offline delivery mode is the subject of further study.
|
Published |
2021-06 |
Edition : 3 |
Number of pages : 190 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 22772:2020 |
Space systems — Requirements of launch vehicle (LV) to electrical ground support equipment (EGSE) interfaces |
This document provides requirements for launch system designers or interface designers regarding interfaces between LV and EGSE, which is used to support on-line processing. It defines electrical interface types, design requirements, environment requirements, verification methods (analyses and tests), and interface check operation requirements.
This document is intended to minimize design costs and reduce risks from errors resulting from miscommunication. It does not limit LV or EGSE organizational requirements to specify a unique interface.
|
Published |
2020-07 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 3184:1998 |
Reach and straddle fork-lift trucks — Stability tests |
|
Withdrawn |
1998-12 |
Edition : 2 |
Number of pages : 11 |
Technical Committee |
53.060
Industrial trucks
|
| ISO 22893:2022 |
Space systems — Software product assurance (SPA) |
This document defines a set of software product assurance requirements in terms of processes and products to be used for the development, maintenance and operation of software for space systems. It provides a uniform basis for defining the software product assurance activities to be applied and maintained throughout the whole software life cycle, from project conception until the software retirement.
This document mainly applies to the space software segment and critical software of ground software segment (e.g. the software which is directly interface to the space segment).
|
Published |
2022-04 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23020:2021 |
Space systems — Determination of test methods to characterize material or component properties required for break-up models used for Earth re-entry |
This document defines the elementary thermal tests to obtain thermal properties of materials and composite materials used to manufacture space body to support the fragmentation and survivability analysis.
This document does not apply to spacecraft containing nuclear power sources[1].
|
Published |
2021-09 |
Edition : 1 |
Number of pages : 16 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23038:2006 |
Space systems — Space solar cells — Electron and proton irradiation test methods |
ISO 23038:2006 specifies the requirements for electron and proton irradiation test methods of space solar cells. It addresses only test methods for performing electron and proton irradiation of space solar cells and not the method for data analysis.
|
Withdrawn |
2006-10 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23038:2018 |
Space systems — Space solar cells — Electron and proton irradiation test methods |
ISO 23038:2018 specifies the requirements for electron and proton irradiation test methods of space solar cells. It addresses only test methods for performing electron and proton irradiation of space solar cells and not the method for data analysis.
|
Published |
2018-02 |
Edition : 2 |
Number of pages : 9 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23041:2007 |
Space systems — Unmanned spacecraft operational procedures — Documentation |
ISO 23041:2007 establishes standards, current guidelines and uniform procedures to minimize duplication of effort between the customer, the agency, participating nations and the emerging commercial space community. ISO 23041:2007 provides recommended practices for the development of space operations and support documentation, which should facilitate the sharing and exchange of beneficial information between organizations involved with space operations. ISO 23041:2007 establishes a common interface to simplify space operations planning and reduce the effort needed to learn and work with new space programmes and support organizations.
|
Withdrawn |
2007-11 |
Edition : 1 |
Number of pages : 26 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23041:2018 |
Space systems — Unmanned spacecraft operational procedures — Documentation |
ISO 23041:2018 establishes standards, current guidelines and uniform procedures to minimize duplication of effort between the customer, the agency, participating nations and the emerging commercial space community. This document provides recommended practices for the development of space operations and support documentation, which should facilitate the sharing and exchange of beneficial information between organizations involved with space operations. This document establishes a common interface to simplify space operations planning and reduce the effort needed to learn and work with new space programmes and support organizations.
|
Published |
2018-04 |
Edition : 2 |
Number of pages : 25 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23103:2020 |
Space link extension — Cross support transfer service — Specification framework |
1.1.1 This Recommended Standard defines, in an abstract manner, a CSTS in terms of:
a) the procedures necessary to provide the service;
b) the states of the service;
c) the behavior of each procedure;
d) the states of the procedures;
e) the operations necessary to constitute the procedures; and
f) the parameters associated with each operation.
1.1.2 It does not specify:
a) individual application services, implementations, or products;
b) the implementation of entities or interfaces within real systems;
c) the methods or technologies required to acquire data;
d) the methods or technologies required to provide a suitable environment for communications; or
e) the management activities required to schedule and configure services.
|
Published |
2020-01 |
Edition : 1 |
Number of pages : 329 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23104:2020 |
Space link extension — Cross support transfer service — Monitored data service |
This Recommended Standard defines the Monitored Data service in terms of:
a) the CSTS procedures that constitute the service;
b) the extensions and refinements of the behavior of those CSTS procedures necessary to provide the transfer service;
c) the extensions and refinements of standard CSTS operations associated with each of the procedures;
d) the relationships among the procedures that constitute the service.
It does not specify:
a) individual implementations or products;
b) the implementation of entities or interfaces within real systems;
c) the methods or technologies required to measure the values of monitored parameters and to detect the occurrence of events of interest;
d) the methods or technologies required for communication;
e) the management activities necessary to schedule, configure, and control the MD-CSTS;
f) the specific parameters that are to be reported and events that are to be notified by the MD-CSTS.
|
Published |
2020-01 |
Edition : 1 |
Number of pages : 108 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23129:2021 |
Space systems — Thermal control coatings for spacecraft — Atomic oxygen protective coatings on polyimide film |
This document defines the general requirements for atomic oxygen (AO) protective coatings that are applied on polyimide thermal control films. It also describes the different properties of coated polyimide films such as indium tin oxide (ITO), SiOx, germanium, and silicone, property measurement test methods, and selection guidelines.
|
Published |
2021-09 |
Edition : 1 |
Number of pages : 19 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23135:2022 |
Space systems — Verification programme and management process |
This document establishes a set of requirements for planning and executing verification programmes for commercial/non-commercial manned and unmanned space systems.
This document defines a distributed verification programme for each contractor that engages in the development of any element of a space system, starting from the lowest level (i.e. unit/piece part level) and the earliest phase (i.e. requirement phase) to the acceptance and the delivery review of a system’s development as well as the launch site activities.
This document primarily addresses verification associated with space, launch, and ground segment acquisitions. Space support segments including range safety, ground support equipment, and launch operation facilities, which are not otherwise addressed in this document, can also benefit from the described verification programme and management processes.
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Published |
2022-03 |
Edition : 1 |
Number of pages : 28 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23230:2023 |
Space systems — Paints and varnishes — Processes, procedures, and requirements for coating materials and coatings |
This document establishes the main requirements for:
— a choice of coating materials and coatings for space applications;
— processes and procedures for the verification of coating materials;
— processes of preparation and quality control of the painted surface;
— the quality control of the applied coatings.
This document also describes the causes of possible defects in coatings.
This document is applicable to coating materials and coatings based on them; it is intended for use by manufacturers of space systems products for various surfaces of spacecraft’s and its constitutive parts (on-board systems, facilities, tools, electronic component base products) with long active lifetimes.
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Published |
2023-01 |
Edition : 1 |
Number of pages : 17 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23312:2022 |
Space systems — Detailed space debris mitigation requirements for spacecraft |
This document defines detailed space debris mitigation requirements and recommendations for the design and operation of unmanned spacecraft in Earth orbit.
This document defines detailed requirements that are applicable to:
a) avoiding the intentional release of space debris into Earth orbit during normal operations;
b) avoiding break-ups in Earth orbit;
c) disposal of a spacecraft after the end of mission;
d) estimating the mass of the remaining usable propellant;
e) developing and maintaining the space debris mitigation plan.
NOTE This document does not cover nuclear power sources on spacecraft.
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Published |
2022-07 |
Edition : 1 |
Number of pages : 21 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23339:2010 |
Space systems — Unmanned spacecraft — Estimating the mass of remaining usable propellant |
ISO 23339:2010 gives requirements for estimating the mass of the remaining usable propellant of an unmanned spacecraft in low Earth orbit (LEO) or geostationary Earth orbit (GEO), and for designing propellant measurement systems. It is applicable to spacecraft with either mono- or bi-propellant propulsion systems using liquid or gaseous chemical propellants, and is limited to such systems because they are the most common for spacecraft in LEOs and GEOs.
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Withdrawn |
2010-12 |
Edition : 1 |
Number of pages : 7 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23460:2011 |
Space projects — Programme management — Dependability assurance requirements |
ISO 23460:2011 presents the requirements for a dependability (reliability, availability and maintainability) assurance programme for space projects.
ISO 23460:2011 defines the dependability requirements for space products as well as for system functions implemented in software, and the interaction between hardware and software.
The provisions of ISO 23460:2011 apply to all programme phases.
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Published |
2011-03 |
Edition : 1 |
Number of pages : 18 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/FDIS 23460 |
Space projects — Programme management — Dependability assurance requirements |
ISO 23460:2011 presents the requirements for a dependability (reliability, availability and maintainability) assurance programme for space projects.
ISO 23460:2011 defines the dependability requirements for space products as well as for system functions implemented in software, and the interaction between hardware and software.
The provisions of ISO 23460:2011 apply to all programme phases.
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Under development |
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Edition : 2 |
Number of pages : 18 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 24246:2022 |
Space systems — Requirements for global navigation satellite system (GNSS) positioning augmentation centers |
This document specifies requirements for GNSS positioning augmentation centres that distribute correction data to provide higher accuracy and integrity information for positioning users in the civil and commercial market.
The GNSS positioning augmentation centres cover the following types of positioning:
a) real-time sub-meter to decimetre-level positioning;
b) real-time centimetre-level positioning;
c) post-processed geodetic positioning.
This document also specifies roles of the following stakeholders and functions of the software present at GNSS positioning augmentation centres:
— role of planner;
— role of designer;
— role of administrator;
— function of software.
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Published |
2022-06 |
Edition : 1 |
Number of pages : 28 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23461:2010 |
Space systems — Programme management — Non-conformance control system |
ISO 23461:2010 specifies a control system for non-conformances related to any product for space systems, such as electrical, electronic, and electromechanical components and software, as well as operational non-conformances and anomalies.
ISO 23461:2010 applies to all deliverable products and supplies, at all levels, which fail to conform to specification requirements and design baselines.
ISO 23461:2010 is applicable throughout phases of: a) procurement, production, qualification, integration, and test; b) acceptance, delivery, and transportation; c) launch preparation and flight or launch readiness; d) operational validation or qualification; e) operation; f) refurbishment.
ISO 23461:2010 also specifies requirements for the interfaces with company internal non-conformance reporting and processing.
Engineering changes lie outside the scope of ISO 23461:2010.
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Published |
2010-06 |
Edition : 1 |
Number of pages : 19 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23462:2014 |
Space systems — Guidelines to define the management framework for a space project |
ISO 23462:2014 provides a framework within which an organization can establish the basis for the development of programme/project management specifications and plans when undertaking the execution of a specific programme/project. It enables the programme/project manager to establish the criteria for programme/project success and to secure the organization's commitment to the programme/project manager's management approach for the overall programme/project and its constituent elements. It includes requirements leading to the establishment of a programme/project management framework, and identification of practices to be applied.
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Published |
2014-04 |
Edition : 1 |
Number of pages : 12 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/TR 23462:2007 |
Space systems — Guidelines to define the management framework for a space project |
ISO/TR 23462:2007 provides a framework within which an organization can establish the basis for the development of programme/project management specifications and plans when undertaking the execution of a specific programme/project. It enables the programme/project manager to establish the criteria for programme/project success and to secure the organization's commitment to the programme/project manager's management approach for the overall programme/project and its constituent elements. It includes guidelines leading to the establishment of a programme/project management framework, and identification of practices to be applied. Following these guidelines also results in traceability of the considerations and decisions on why and how the programme/project is conducted according to its specific characteristics.
ISO/TR 23462:2007 provides a holistic approach for programme/project managers to apply their organization's programme/project management practices when defining the management framework for programme/project planning. It is based on a systematic method of
defining the programme/project objectives and success criteria,
identifying and elaborating the specific characteristics of their programme/project,
specifying the management elements needed,
establishing and agreeing the management approaches to be implemented,
compiling these into a programme/project management framework document.
The guidelines in ISO/TR 23462:2007 are applicable to any organization undertaking the execution of space programmes/projects.
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Withdrawn |
2007-07 |
Edition : 1 |
Number of pages : 10 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23569:2021 |
Space systems — Spacecraft system level radio frequency (RF) performance test in compact range |
This document specifies the verification test activities for assessing the RF performance of integrated spacecraft, including test items, test requirements, and typical test procedures, test facility and chamber environment, with respect to the testing using compact range. This document is applicable to the RF performance test for spacecraft at system level using compact range.
|
Published |
2021-11 |
Edition : 1 |
Number of pages : 44 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 23670:2021 |
Space systems — Vibration testing |
This document provides guidance and requirements for test providers and interested parties to implement vibration testing.
This document specifies methods, including the force limiting approach, to mitigate unnecessary over-testing of spacecraft, subsystems and units for space application.
The technical requirements in this document can be tailored to meet the actual test objectives.
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Published |
2021-09 |
Edition : 1 |
Number of pages : 28 |
Technical Committee |
17.160
Vibrations, shock and vibration measurements
;
49.140
Space systems and operations
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| ISO 23835:2022 |
Space Systems — Mechanism design and verification |
This document establishes requirements for the design, material selection and characterization, fabrication, testing and inspection of all space mechanisms on spacecraft and payloads to meet the mission performance requirements. This document does not cover the requirements for mechanisms on expendable and reusable launch vehicles. Applicability of the requirements contained in this document to launch vehicle mechanisms is a decision left to the individual launch vehicle project.
This document applies specifically to all moving mechanisms used in spacecraft during all phases of the mission, with the exception of engines and thermal protection systems.
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Published |
2022-04 |
Edition : 1 |
Number of pages : 32 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 24917:2010 |
Space systems — General test requirements for launch vehicles |
ISO 24917:2010 establishes general test requirements for launch vehicles equipped with liquid-propellant engines, launched from stationary ground-, sea- and air-based launchers, in all phases of their development.
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Withdrawn |
2010-10 |
Edition : 1 |
Number of pages : 35 |
Technical Committee |
49.140
Space systems and operations
|
| ISO/TR 23989:2020 |
Space environment (natural and artificial) — Operational estimation of the solar wind energy input into the Earth's magnetosphere by means of the ground-based magnetic polar cap (PC) index |
This document provides guidelines for specifying the qualitative estimation of the solar wind energy input into the magnetosphere with use of operative ground-based information on the polar cap magnetic activity (PC index).
The solar wind energy incoming into the magnetosphere predetermines development of the magnetospheric disturbances: magnetic storms and substorms. Magnetospheric disturbances include a wide range of phenomena and processes directly affecting human activity, such as satellite damage, radiation hazards for astronauts and airline passengers, telecommunication problems, outrages of power and electronic systems, effects in the atmospheric processes, and impact on human health.
This document is intended for on-line monitoring the magnetosphere state and nowcasting the intensity and extent of magnetic disturbances as well as parameters of the high-latitude ionosphere. The method and accuracy of estimating is ascertained by close relationship between the PC index and interplanetary electric field (as the most geoeffective solar wind parameter), on the one hand, and between the PC index and magnetoshpheric disturbances, on the other hand.
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Published |
2020-01 |
Edition : 1 |
Number of pages : 11 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 24113:2010 |
Space systems — Space debris mitigation requirements |
ISO 24113:2010 defines the primary space debris mitigation requirements applicable to all elements of unmanned systems launched into, or passing through, near-Earth space, including launch vehicle orbital stages, operating spacecraft and any objects released as part of normal operations or disposal actions.
The requirements contained in ISO 24113:2010 aim to reduce the growth of space debris by ensuring that spacecraft and launch vehicle orbital stages are designed, operated and disposed of in a manner that prevents them from generating debris throughout their orbital lifetime.
ISO 24113:2010 is the top-level standard in a series of standards addressing debris mitigation. It will be the main interface for the user, bridging between the primary debris mitigation requirements and the lower level implementation standards that will ensure compliance.
ISO 24113:2010 does not cover launch phase safety for which specific rules are defined elsewhere.
|
Withdrawn |
2010-07 |
Edition : 1 |
Number of pages : 13 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 24113:2011 |
Space systems — Space debris mitigation requirements |
ISO 24113:2011 defines the primary space debris mitigation requirements applicable to all elements of unmanned systems launched into, or passing through, near-Earth space, including launch vehicle orbital stages, operating spacecraft and any objects released as part of normal operations or disposal actions.
The requirements contained in ISO 24113:2011 are intended to reduce the growth of space debris by ensuring that spacecraft and launch vehicle orbital stages are designed, operated and disposed of in a manner that prevents them from generating debris throughout their orbital lifetime.
ISO 24113:2011 is the top-level standard in a family of standards addressing debris mitigation. It will be the main interface for the user, bridging between the primary debris mitigation requirements and the lower-level implementation standards that will ensure compliance.
ISO 24113:2011 does not cover launch phase safety for which specific rules are defined elsewhere.
|
Withdrawn |
2011-05 |
Edition : 2 |
Number of pages : 13 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 24113:2019 |
Space systems — Space debris mitigation requirements |
This document defines the primary space debris mitigation requirements applicable to all elements of unmanned systems launched into, or passing through, near-Earth space, including launch vehicle orbital stages, operating spacecraft and any objects released as part of normal operations.
The requirements contained in this document are intended to reduce the growth of space debris by ensuring that spacecraft and launch vehicle orbital stages are designed, operated and disposed of in a manner that prevents them from generating debris throughout their orbit lifetime. The requirements are also intended to reduce the casualty risk on ground associated with atmospheric re-entry of space objects.
This document is the top-level standard in a family of standards addressing space debris mitigation. It is the main interface for the user, bridging between the primary space debris mitigation objectives and a set of lower level standards and technical reports that support conformance. The lower level documents contain detailed requirements and implementation measures associated with the high-level requirements in this document.
|
Published |
2019-07 |
Edition : 3 |
Number of pages : 13 |
Technical Committee |
49.140
Space systems and operations
|
| ISO 24113 |
Space systems — Space debris mitigation requirements |
This document defines the primary space debris mitigation requirements applicable to all elements of unmanned systems launched into, or passing through, near-Earth space, including launch vehicle orbital stages, operating spacecraft and any objects released as part of normal operations.
The requirements contained in this document are intended to reduce the growth of space debris by ensuring that spacecraft and launch vehicle orbital stages are designed, operated and disposed of in a manner that prevents them from generating debris throughout their orbit lifetime. The requirements are also intended to reduce the casualty risk on ground associated with atmospheric re-entry of space objects.
This document is the top-level standard in a family of standards addressing space debris mitigation. It is the main interface for the user, bridging between the primary space debris mitigation objectives and a set of lower level standards and technical reports that support conformance. The lower level documents contain detailed requirements and implementation measures associated with the high-level requirements in this document.
|
Under development |
|
Edition : 4 |
|
Technical Committee |
49.140
Space systems and operations
|
| ISO/FDIS 24245 |
Space systems — Global Navigation Satellite System (GNSS) receiver class codes |
|
Under development |
|
Edition : 1 |
Number of pages : 17 |
Technical Committee |
49.140
Space systems and operations
|