49.140 航天系统和操作装置 标准查询与下载

BS EN 16603-10-03:2022 空间工程 测试

1   Scope This standard addresses the requirements for performing verification by testing of space segment elements and space segment equipment on ground prior to launch. The document is applicable for tests performed on qualification models, flight models (tested at acceptance level ) and protoflight models. The standard provides: • Requirements for test programme and test management, • Requirements for retesting, • Requirements for redundancy testing, • Requirements for environmental tests , • General requirements for functional and performance tests , NOTE 1 Specific requirements for functional and performance tests are not part of this standard since they are defined in the specific project documentation. • Requirements for qualification, acceptance, and protoflight testing including qualification, acceptance, and proto-fight models’ test margins and duration,

Space engineering. Testing

BS EN 16603-50-25:2022 航天工程 CCSDS 232.0-B-3、TC 空间数据链路协议的采用通知

Space engineering - Adoption Notice of CCSDS 232.0-B-3, TC Space Data Link Protocol

BS ISO 24411:2022 空间系统 微振动测试

1   Scope This document specifies requirements for the implementation of spacecraft level micro-vibration tests on space systems to be considered by test providers, including test designers and test engineers. It also gives guidance for spacecraft designers and interested parties. The spacecraft level micro-vibration test is applicable to space systems which contain payload equipment sensitive to the micro-vibration environment which only induced by the internal disturbance sources on-orbit, e.g. for the purpose of earth observation, space telescopes, optical experiments, telecommunication.

Space systems. Micro-vibration testing

ISO 15388:2022 航天系统.污染和清洁度控制

Space systems — Contamination and cleanliness control

ISO 15865:2022 航天系统.鉴定评估

This document es tablishes general rules for qualification assessment of space s ys tems and products used in space s ys tems against their functional and technical specifications . It es tablishes general requirements for determining s ys tem or product readiness for any s tage of the life cycle. This includes, for example, readiness for development, manufacture, tes t, operation, modification, or disposal. This document is applicable to s ys tems and products used in flight or ground support and to products at all levels in a product tree. It applies to s ys tems and products consis ting of hardware, software, facilities, materials, methods, processes, procedures or any combination of these. It es tablishes common: a) general requirements for qualification assessment of item readiness; b) approaches to qualification. This document is intended for use as the basis for a design j us tification plan. It is intended to be used either in es tablishing an agreement for such a plan between a customer and a supplier or as the basis for a supplier’s internal qualification practices.

Space systems — Qualification assessment

ISO 24411:2022 航天系统.微振动试验

This document specifies requirements for the implementation of spacecraft level micro-vibration tests on space s ys tems to be considered by test providers, including test designers and test engineers. It also gives guidance for spacecraft designers and interes ted parties . The spacecraft level micro-vibration test is applicable to space s ys tems which contain payload equipment sensitive to the micro-vibration environment which only induced by the internal dis turbance sources on-orbit, e.g. for the purpose of earth observation, space telescopes, optical experiments, telecommunication.

Space systems — Micro-vibration testing

EN 16603-10-03:2022 航天工程.检验

This standard addresses the requirements for performing verification by testing of space segment elements and space segment equipment on ground prior to launch. The document is applicable for tests performed on qualification models, flight models (tested at acceptance level) and protoflight models. The standard provides: • Requirements for test programme and test management, • Requirements for retesting, • Requirements for redundancy testing, • Requirements for environmental tests, • General requirements for functional and performance tests, NOTE Specific requirements for functional and performance tests are not part of this standard since they are defined in the specific project documentation. • Requirements for qualification, acceptance, and protoflight testing including qualification, acceptance, and protofight models’ test margins and duration, • Requirements for test factors, test condition, test tolerances, and test accuracies, • General requirements for development tests pertinent to the start of the qualification test programme, NOTE Development tests are specific and are addressed in various engineering discipline standards. • Content of the necessary documentation for testing activities (e.g. DRD). Due to the specific aspects of the follow ing types of test, this Standard does not address: • Space system testing (i.e. testing above space segment element), in particular the system validation test, • In-orbit testing, • Testing of space segment subsystems, NOTE Tests of space segment subsystems are often limited to functional tests that, in some case, are run on dedicated models. If relevant, qualification tests for space segment subsystems are assumed to be covered in the relevant discipline standards. Testing of hardware below space segment equipment levels (including assembly, parts, and components), • Testing of stand-alone software, NOTE For verification of flight or ground softw are, EN 16603-40 (ECSS-E-ST-40) and EN 16602-80 (ECSS-Q-ST-80) apply. • Qualification testing of tw o-phase heat transport equipment, NOTE For qualification testing of tw o-phase heat transport equipment, EN 16603-31-02 (ECSS-E-ST-31-02) applies. • Tests of launcher segment, subsystem and equipment, and launch facilities, • Tests of facilities and ground support equipment, • Tests of ground segment. This activity will be the update of EN16603-10-03:2014 NOTE: Parallel development of update of EN Standard and the new European TR17603-10-03.

Space engineering - Testing

BS EN 16603-35-06:2022 空间工程 航天器推进硬件的清洁度要求

1   Scope ECSS‑E‑ST‑35‑06 belongs to the Propulsion field of the mechanical discipline, and concerns itself with the cleanliness of propulsion components, sub-systems and systems The standard • defines design requirements which allow for cleaning of propulsion components sub-systems and systems and which avoid generation or unwanted collection of contamination, • identifies cleanliness requirements (e.g. which particle  / impurity / wetness level can be tolerated), • defines requirements on cleaning to comply with the cleanliness level requirements, and the requirements on verification, • identifies the cleanliness approach, cleaning requirements, (e.g. what needs to be done to ensure the tolerable level is not exceeded, compatibility requirements), • identifies, specifies and defines the requirements regarding conditions under which cleaning or cleanliness verification takes place (e.g. compatibility, check after environmental test). The standard is applicable to the most commonly used propulsion systems and their related storable propellant combinations: Hydrazine (N 2 H 4 ), Mono Me...

Space engineering. Cleanliness requirements for spacecraft propulsion hardware

BS EN 16603-50-21:2022 空间工程 CCSDS 131.0-B-3、TM 同步和信道编码的采用通知

1   Scope This document identifies the clauses and requirements modified with respect to the standard CCSDS 131.0‑B‑3, TM Synchronization and Channel Coding , Issue 3, September 2017 for application in ECSS.

Space engineering. Adoption Notice of CCSDS 131.0-B-3, TM Synchronization and Channel Coding

22/30459339 DC BS ISO 27852 空间系统 轨道寿命估计

BS ISO 27852. Space systems. Estimation of orbit lifetime

BS EN 16603-50-26:2022 空间工程 CCSDS 232.1-B-2 通信操作程序-1的采用通知

Space engineering. Adoption Notice of CCSDS 232.1-B-2, Communications Operation Procedure-1

BS EN 16603-50-24:2022 空间工程 CCSDS 231.0-B-3、TC 同步和信道编码的采用通知

Space engineering. Adoption Notice of CCSDS 231.0-B-3, TC Synchronization and Channel Coding

ISO 16378:2022 航天系统.热控制材料的热光特性测量

This document specifies the multiple measurement methods, instruments, equipment, and samples used to calculate the thermo-optical properties of thermal control materials. This document compares their features, indicates their limitations and biases, and guides the applications. This document also defines requirements for calibration and reference materials to ensure data quality. This document specifies the following test methods, including the configuration of samples and calculations. a) Solar absorptance using a spectrophotometer (αs ) — Annex A. b) Solar absorptance using the comparative test method (αp ) — Annex B. c) Hemispherical infrared emittance using the thermal test method (εh-t ) — Annex C. d) Normal infrared emittance using an IR spectrometer (εn-s ) — Annex D. e) Normal infrared emittance using ellipsoid collector optics (εn-e ) — Annex E. f) Normal infrared emittance using two rotating cavities (εn-c ) — Annex F.

Space systems — Measurements of thermo-optical properties of thermal control materials

BS EN 16603-50:2022 空间工程 通讯

1   Scope This Standard specifies the requirements for the development of the end-to-end data communications system for spacecraft. Specifically, this standard specifies: • The terminology to be used for space communication systems engineering. • The activities to be performed as part of the space communication system engineering process, in accordance with the ECSS‑E‑ST‑10 standard. • Specific requirements on space communication systems in respect of functionality and performance. The communications links covered by this Standard are the space-ground (i.e. space-to-ground and ground-to-space) and space-to-space links used during spacecraft operations, and the communications links to the spacecraft used during the assembly, integration and test, and operational phases. Spacecraft end-to-end communication systems comprise components in three distinct domains, namely the ground network, the space link, and the space network. This Standard covers the components of the space link and space network in detail. However, this Standard only covers those aspects of the ground network that are necessary for the provision of the end-to-end communication services . NOTE Other aspects of the ground network are covered in EC...

Space engineering. Communications

CEN/CLC/TR 17603-10-03:2022 空间工程 测试指南

This handbook provides additional information for the application of the Testing standard EN 16603-10-03. This handbook will be the guideline for all space projects, related equipment and complete systems, by providing background information that aids the reader to better understand and meet the requirements of the standard. The document would follow the flow of the Testing standard and in particular w hatever is excluded from the testing standard (see Scope of EN 16603-10-03) should also be excluded. NOTE: EN 16603-10-03:2014 will be in parallel also updated to take into account the new TR.

Space engineering - Testing guidelines

BS ISO 23312:2022 空间系统 航天器的详细空间碎片减缓要求

1   Scope 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.

Space systems. Detailed space debris mitigation requirements for spacecraft

22/30455890 DC BS EN 16603-20-08 空间工程 光伏组件和组件

BS EN 16603-20-08. Space engineering. Photovoltaic assemblies and components

22/30441490 DC BS ISO 17689 空间系统 地面系统、地面支持设备和带有效载荷的运载火箭之间的接口控制文件

BS ISO 17689. Space systems. Interface control documents between ground systems, ground support equipment and launch vehicle with payload

BS EN 16603-50-23:2022 空间工程 CCSDS 732.0-B-3、AOS 空间数据链路协议的采用通知

Space engineering. Adoption Notice of CCSDS 732.0-B-3, AOS Space Data Link Protocol

BS EN 16603-50-22:2022 空间工程 CCSDS 132.0-B-2、TM 空间数据链路协议的采用通知

Space engineering. Adoption Notice of CCSDS 132.0-B-2, TM Space Data Link Protocol