• sale 15% off
    • Draft
      3 pages
      English language
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    • Standard
      3 pages
      English language
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    • Draft
      3 pages
      English language

This document contains information on the design and operational practices for launch vehicle orbital stages for mitigating space debris. This document provides information to engineers on what are required or recommended in the family of space debris mitigation standards to reduce the growth of space debris by ensuring that spacecraft is designed, operated, and disposed of in a manner that prevents them from generating debris throughout their orbital lifetime.

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    • Technical report
      56 pages
      English language
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    • Draft
      56 pages
      English language

This document provides detailed information on the various methods of assessing the health status of lithium-ion space batteries in flight and makes recommendations to battery suppliers, spacecraft manufacturers and operators to ease this assessment.

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    • Draft
      54 pages
      English language
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    • Technical report
      54 pages
      English language

This document specifies criteria and requirements for the use of explosive systems and explosive devices commonly used on spacecraft and other space products, including launch vehicles and space vehicle systems. It addresses the aspects of design, analysis, verification, manufacturing, operations and safety. To the greatest extent possible, requirements from past and existing standards have been analyzed, selected and tailored to be incorporated herein. In addition, the requirements herein inclu...view more

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    • Draft
      77 pages
      English language
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    • Standard
      77 pages
      English language

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.

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    • Standard
      37 pages
      English language
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    • Draft
      37 pages
      English language

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 organizatio...view more

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    • Standard
      10 pages
      English language
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    • Draft
      10 pages
      English language

This document presents the requirements for requirements management (RM) for space projects. This document addresses the space programme/project management requirements, applicable through a top-down approach in a contractual relationship between customers and suppliers. The objective of this document is to state and establish a common reference framework for all the customers and suppliers in the space sector to deploy requirements management for all space products and projects. This document o...view more

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    • Standard
      15 pages
      English language

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.

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    • Standard
      20 pages
      English language

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.

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    • Standard
      47 pages
      English language

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 ...view more

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    • Technical report
      11 pages
      English language

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, pr...view more

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    • Standard
      15 pages
      English language

This document specifies the methods used for estimating geomagnetic indices for time intervals ranging from short-term (hours to a few months) to long-term (months to years). This document is intended for use to predict future geomagnetic indices and space environment.

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    • Standard
      25 pages
      English language

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

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    • Standard
      41 pages
      English language

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 ...view more

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    • Standard
      13 pages
      English language

This document specifies requirements for the following: — planning for disposal of a spacecraft operating at geosynchronous altitude to ensure that final disposal is sufficiently characterized and that adequate propellant will be reserved for the manoeuvre; — selecting final disposal orbits where the spacecraft will not re-enter the operational region within the next 100 years; — executing the disposal manoeuvre successfully; — depleting all energy sources on board the vehicle before the end of ...view more

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    • Standard
      46 pages
      English language

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.

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    • Standard
      40 pages
      English language

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 activ...view more

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    • Standard
      7 pages
      English language

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 app...view more

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    • Standard
      22 pages
      English language

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.

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    • Standard
      29 pages
      English language

ISO 21494:2019 specifies magnetic test methods including magnetic field test methods, magnetic moment test methods, magnetization and demagnetization test methods and magnetic compensation test methods. This document is applicable to magnetic tests on several levels: spacecraft-level, subsystem-level and unit-level. ISO 21494:2019 gives guidelines for conducting magnetic tests both in zero-magnetic field environment provided by magnetic test facilities and in the presence of the geomagnetic fiel...view more

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    • Standard
      27 pages
      English language

This document provides a framework with which to assess, reduce, and control the potential risks that spacecraft and launch vehicle orbital stages (referred to hereinafter as "space vehicles") pose to people and the environment when those space vehicles re-enter the Earth's atmosphere and impact the Earth's surface. It is intended to be applied to the planning, design, and review of space vehicle missions for which controlled or uncontrolled re-entry is inevitable. This document is applicable to...view more

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    • Standard
      23 pages
      English language

This document (first level standard) is the main document among the others regarding human-life activity support systems and equipment integration in space flight. This document, along with second and third level standards, forms a complex three-level international standard entitled: Space systems — Human-life activity support systems and equipment integration in space flight. It is applicable to all human space flight programmes in all manned space objects, including space systems, space statio...view more

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    • Standard
      7 pages
      English language

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. ...view more

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    • Standard
      36 pages
      English language

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 fo...view more

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    • Technical specification
      18 pages
      English language

This document describes the set of management requirements needed to identify and provide logistic support, so the customer can operate and maintain a product in its operational environment for the expected lifetime. These requirements also aim, throughout the product life cycle, at implementing everything pertinent to the control of risks considered as critical for operational objectives. The management requirements are applicable to those activities necessary to design, develop, deliver, deplo...view more

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    • Standard
      23 pages
      English language

This document defines the requirements and verification methods from design to on-orbit operation for Satellite Based Passive Microwave Sensors. This document covers the requirements for, design, analysis, manufacturing, ground tests and on-orbit self-sensor calibration and validation. In addition, this document includes the conditions considered for on-orbit inter-comparison among sensors as preparation for cross-calibration. This document includes some examples on how to apply the development ...view more

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    • Standard
      26 pages
      English language

This document describes minimum requirements for small spacecraft. Small spacecraft may employ untraditional spacecraft development and management philosophy. These spacecraft projects are usually budget-limited or mass-limited, which makes a single (exclusive) launch unaffordable. The scope of this document encompasses different categories of small spacecraft — so-called mini-, micro-, nano-, pico- and femto-, as well as CubeSat, spacecraft. Therefore, for the sake of convenience, the term "sma...view more

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    • Technical specification
      6 pages
      French language
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    • Technical specification
      6 pages
      English language

This document is a second level standard is one of the several others regarding human-life activity support systems and equipment integration in space flight. This document, along with first and third level standards, form a complex three-level international standard entitled "Space systems — Human-life activity support systems and equipment integration in space flight". It is applicable to human space flight programs in all manned space objects, including spacecraft, space stations, lunar and p...view more

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    • Standard
      7 pages
      English language

This document specifies requirements for the design and verification of fibre optic components used in space fibre optic sub-systems. In this document, the requirements are established to assure the reliability and environmental adaptability of fibre optic components in space environmental conditions. These are in a range of applications such as ground systems, unmanned applications and manned systems. This document suggests a set of requirements to be applied to the selection of space fibre opt...view more

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    • Standard
      17 pages
      English language

This document defines the programme management requirements for material, mechanical parts and processes for projects covering mission definition, design, development, production and operations of space systems, including disposal. This document covers the following: — management, including organization, reviews, acceptance status and documentation control; — selection criteria and rules; — evaluation, validation and qualification, or verification testing; — procurement and receiving inspection;...view more

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    • Standard
      46 pages
      English language

ISO 16726:2018 is a 3rd level standard with respect to ISO 17763 and is a 2nd level standard with respect to ISO 16157. ISO 16726:2018 establishes environmental conditions for spacecraft air quality, including harmful chemical contaminants and requirements for harmful air contaminants' removal systems. NOTE These systems support stated environmental conditions.

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    • Standard
      10 pages
      English language

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...view more

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    • Standard
      25 pages
      English language

ISO/TS 18667:2018 applies to the design, development, fabrication, test, and operation of commercial, civil, and military space and ground control systems, sites/facilities, services, equipment, and computer software. Criteria is provided for rating the capability of the entire SD&QA programme or an individual SD&QA process to identify, assess, and eliminate or mitigate risks that threaten safety or mission success. The predefined capability rating criteria define the sequence of activities nece...view more

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    • Technical specification
      67 pages
      English language

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.

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    • Standard
      9 pages
      English language

ISO 20892:2017 specifies procedures in the preparation and carrying out of the modernization process of launch complexes and their components. These procedures are devised in case there is a need to make changes in existing configuration of launch complexes. ISO 20892:2017 establishes the following: a) modernization stages; b) modernization performance requirements; c) functions of the main participants of the modernization process and their interactions. The requirements specified in this docum...view more

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    • Standard
      7 pages
      English language

ISO 19971:2018 provides general format for spacecraft and launch vehicle Combined Operation Plan (COP).

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    • Standard
      15 pages
      English language

ISO 20188:2018 provides the recommended practices of product assurance (PA) requirements applicable to commercial satellite.

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    • Standard
      34 pages
      English language

ISO 18676:2017 presents the guidelines for the management of systems engineering for space systems. ISO 18676:2017 addresses the systems engineering activities and provides guidelines for interfacing with specific major management subjects (e.g. configuration management, data management, interface management, risk management, requirements management, and integrated logistics support), which are themselves the subject of this document. ISO 18676:2017 establishes a common reference for all custome...view more

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    • Standard
      17 pages
      English language

ISO 18322:2017 specifies requirements for when a space test centre needs to demonstrate its competence to consistently provide space testing that meets customer requirements. It specifies requirements for space test centres, applicable to the test process, test personnel (both, of the customer and the space test centre), test facilities, test environment and any operations related to the test item under responsibility of the space test centre as requested by the customer. ISO 18322:2017 also def...view more

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    • Standard
      23 pages
      English language

ISO 19924:2017 provides guidance for test providers and interested parties to implement acoustic tests of aerospace systems, subsystems, modules and units for applicable spacecraft programs. ISO 19924:2017 specifies a framework to meet test and process requirements and acts as a supplement to ISO 15864. The acoustic test system, the technical requirements and the procedures for acoustic tests in reverberant chambers are described. Furthermore, the criteria for the manual test interruption and ev...view more

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    • Standard
      17 pages
      English language

ISO 19683:2017 provides test methods and test requirements for design qualification and/or acceptance of small spacecraft or units. It provides the minimum test requirements and test methods to qualify the design and manufacturing methods of commercial small spacecraft and their units and to accept the final products. ISO 19683:2017 places emphasis on achieving reliability against infant mortality after satellite launch to orbit while maintaining low cost and fast delivery. ISO 19683:2017 is app...view more

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    • Standard
      85 pages
      English language

ISO 17770:2017 addresses CubeSats, CubeSat Deployer and related verification of assurance/quality terms and metrics. ISO 17770:2017 defines a unique class of picosatellite, the CubeSat. CubeSats are ideal as space development projects for universities around the world. In addition to their significant role in educating space scientists and engineers, CubeSats provide a low-cost platform for testing and space qualification of the next generation of small payloads in space. A key component of the ...view more

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    • Standard
      9 pages
      English language

ISO 19923:2017 specifies space plasma environments that lead to the generation of the worst-case surface potential differences for spacecraft. It also specifies how to estimate worst-case potential differences by using the simulation codes provided. ISO 19923:2017 includes plasma energy and density in GEO, PEO, and MEO. ISO 19923:2017 does not include descriptions of plasma energy and density in LEO because large surface charging in LEO is likely to be due to high-voltage power generation by ins...view more

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    • Standard
      14 pages
      English language

ISO 16192:2017 outlines lessons learned principles and guidelines that are applicable in all space project activities (management, technical, quality, cost and schedule). The application of this document is intended to be included in the supplier quality management system, but can be tailored in individual contracts as agreed by the customer and supplier, depending on: - the content of each project (size, technological level and novelty, particular organization, participants, etc.); - the intere...view more

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    • Standard
      13 pages
      English language

ISO 19826:2017 defines management requirements of product characteristics, including their classification, in order to highlight those areas of the product to which specific attention, control or inspections are applied. ISO 19826:2017 is applicable to direct implementation of space product characteristic management, especially for mechanical parts and fluidic equipment.

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    • Standard
      13 pages
      English language

ISO/TR 20590:2017 contains non-normative information on the design and operational practices for launch vehicle orbital stages for mitigating space debris. ISO/TR 20590:2017 can be used to guide engineers in the application of the family of space debris mitigation standards (see 4.2) to reduce the growth of space debris by ensuring that launch vehicle orbital stages are designed, operated, and disposed of in a manner that prevents them from generating debris throughout their orbital lifetime.

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    • Technical report
      33 pages
      English language

ISO 17540:2016 provides terms and definitions in scope of design, testing, reliability analysis and quality control of liquid rocket engines. The terms are required for use in all types of documentation and literature including in the scope of standardization or using the results of this activity.

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    • Standard
      32 pages
      English language

ISO 18257:2016 specifies the basic design requirements for semiconductor ICs for space applications, including its design process, as well as required tasks and requirements of each stage. Requirements of specific circuit design are not included.

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    • Standard
      24 pages
      English language

ISO 17666:2016 defines, extending the requirements of ISO 14300‑1, the principles and requirements for integrated risk management on a space project. It explains what is needed to implement a project-integrated risk management policy by any project actor, at any level (i.e. customer, first-level supplier, or lower-level suppliers). It contains a summary of the general risk management process, which is subdivided into four (4) basic steps and nine (9) tasks. The implementation can be tailored to ...view more

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    • Standard
      20 pages
      English language