V70 航天器综合 标准查询与下载

GB/T 29081-2012 航天器模态计算方法

本标准规定了航天器的模态计算方法、本标准适用于航天器的模态计算和航天器界面广义刚度矩阵和广义质量矩阵的计算、舱段、组件的模态计算可参照使用、

Modal analysis for spacecraft

GB/T 32296-2015(英文版) 运载火箭和航天器的通用参考系

General reference frames for launch vehicle and spacecraft

ISO 24638:2021 航天系统. 压力部件和压力系统集成

This document establishes the baseline requirements for the design, fabrication and testing of space flight pressure components. It also establishes the requirements for the assembly, installation, test, inspection, operation and maintenance of the pressure systems in spacecraft and launch vehicles. These requirements, when implemented on a particular space system, ensure a high level of confidence in achieving safe and reliable operation. This document applies to all pressure components other than pressure vessels and pressurized structures in a pressure system. It covers lines, fittings, valves, bellows, hoses and other appropriate components that are integrated to form a pressure system. The requirements for pressure vessels and pressurized structures are set forth in ISO 14623. This document does not apply to engine components.

Space systems - Pressure components and pressure system integration

BS EN 16603-31-02:2018 航天工程. 两相热传输设备

Space engineering. Two-phase heat transport equipment

DIN EN 9136:2018 航空航天系列. 根本原因分析与问题解决（9S方法论）; 德文和英文版本 EN 9136-2018

The objective of any organization, as part of continual improvement, is to reduce the number of issues (i.e., undesirable conditions, defects, failures) and to minimize their impact on quality, delivery performance, and cost. For this purpose it should have adequate processes. This Standard includes, with the 9S Methodology, a methodology to improve the way escapes and issues are managed, including communication between all parties [e. g., engineering, Materials Review Board (MRB), manufacturing, manufacturing engineering, supplier, customer] to reduce their impact, contain them as far upstream as possible, and prevent recurrence.

Aerospace series - Root cause analysis and problem solving (9S Methodology); German and English version EN 9136:2018

ISO 19923:2017 空间环境（自然和人工）.航天器最坏情况电势差产生的等离子体环境

This document 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. This document includes plasma energy and density in GEO, PEO, and MEO. This document 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 instrumentation of the spacecraft. This document deals with external surface charging of spacecraft only.

Space environment (natural and artificial) - Plasma environments for generation of worst case electrical potential differences for spacecraft

ISO 17770:2017 航天系统. 立方体卫星(CubeSats)

This document addresses CubeSats, CubeSat Deployer and related verification of assurance/quality terms and metrics. This document 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 project is the development of a standard CubeSat Deployer. This Deployer is capable of releasing a number of CubeSats as secondary payloads on a wide range of launchers. The standard Deployer requires all CubeSats to conform to common physical requirements, and share a standard Deployer interface. CubeSat development time and cost can be significantly reduced by the development of standards that are shared by a large number of spacecraft. Normative control of the CubeSat design, qualification and acceptance testing is generally applied from other small satellite specific standards with the exception of CubeSat/Deployer launch environment test.

Space systems - Cube satellites (CubeSats)

BS ISO 22645:2016 航天数据和信息传送系统.TM(遥测技术)航天数据链接协议

Space data and information transfer systems. TM (telemetry) space data link protocol

ISO 18257:2016 航空航天系统. 航空航天应用的半导体集成应用. 设计要求

This document specifies the basic design requirements for semiconductor ICs for space applications, includingits design process, as well as required tasks and requirements ofeach stage. Requirements of specific circuit design are not included.

Space systems - Semiconductor integrated circuits for space applications - Design requirements

BS ISO 17851:2016 航天系统. 材料试验用航天环境模拟. 通用原则和标准

Space systems. Space environment simulation for material tests. General principles and criteria

NF L90-200-60*NF EN 16602-60:2016 航天产品保证. 电气, 电子和机电 (EEE) 元器件

Space product assurance - Electrical, electronic and electromechanical (EEE) components

NF L90-200-60-02*NF EN 16602-60-02:2016 航天产品保证. ASIC和FPGA开发

Space product assurance - ASIC and FPGA development

BS ISO 17761:2015 航天环境 (天然和人造). 低海拔 (300 km至600 km) 的高能量辐射模型

Space environment (natural and artificial). Model of high energy radiation at low altitudes (300 km to 600 km)

BS ISO 22642:2015 航天数据和信息传送系统.TC同步和信道编码

Space data and information transfer systems. TC synchronization and channel coding

ISO 18238:2015 航天系统. 闭环问题解决的管理

Space systems - Closed loop problem solving management

BS ISO 16679:2015 空间系统. LV/SC分离后的相对涌动分析元素

Space systems. Relative motion analysis elements after LV/SC separation

BS EN 16603-31-02:2015 航天工程. 两相热传输设备

Space engineering. Two-phase heat transport equipment

EN 16602-70-55:2015 航天产品保证.飞行硬件和洁净室微生物学检验

Space product assurance - Microbiological examination of flight hardware and cleanrooms

EN 16603-31-02:2015 空间工程.两相热传输设备

Space engineering - Two-phase heat transport equipment

EN 16602-70-56:2015 航天产品保证.飞行硬件气相生物负荷的降低

Space product assurance - Vapour Phase Bioburden Reduction for Flight Hardware