ISO 19683:2017由国际标准化组织 IX-ISO 发布于 2017-08-14。
ISO 19683:2017在国际标准分类中归属于: 49.140 航天系统和操作装置。
ISO 19683:2017 空间系统 - 小型航天器和装置的设计鉴定和验收试验的最新版本是哪一版?
最新版本是 ISO 19683:2017 。
* 在 ISO 19683:2017 发布之后有更新,请注意新发布标准的变化。
This document 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. This document places emphasis on achieving reliability against infant mortality after satellite launch to orbit while maintaining low cost and fast delivery. This document is applied to satellites whose development methods are different from the ones used for traditional satellites that have little room for risk tolerance, as shown in Figure 1. 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 “small spacecraft” is used throughout this document as a generic term. This document includes CubeSat, as long as it is developed with the untraditional processes. Figure 1 — Applicability of this document This document does not cover satellite deployment mechanisms, such as POD, as the verification requirements are defined in the Interface Control Document (ICD) with the launcher, such as ISO 26869. This document does not cover software testing, although some tests such as functional test, mission test and end-to-end test are inherently used to test the software installed in the hardware being tested. General requirements and processes of satellite software testing can be found in various references, such as ECSS-E-ST40. This document does not cover requirements regarding safety nor debris mitigation. Appropriate documents such as ISO 14620–1 or ISO 24113 can be referred to. Other common requirements for small spacecraft can be found in Reference [14].
在复杂的太空环境中,高能质子是空间辐射的重要来源,且能穿透航天器外壳进入航天器内部,对航天器的芯片和材料造成辐射损伤,对航天员的健康和航天设备的正常工作构成严重威胁。若能在地面通过相关装置模拟出太空的辐射环境,开展相关研究,就能更方便地对辐射环境进行控制,对辐射过程相关参数进行监测,更加深入地了解空间辐射环境效应的规律特征。...
“空间环境地面模拟装置”国家重大科技基础设施是国家发展改革委批准立项的“十二五”期间重点规划项目,由哈尔滨工业大学和航天科技集团联合建设,旨在聚焦航天领域重大基础性科学技术问题,构建我国首个空间综合环境与航天器、生命体和等离子体作用科学领域的大型研究基地,形成国际领先水平的空间环境耦合效应试验研究平台。...
NASA的初步计划包括研发一种装备了超音速冲压式喷射发动机的楔形航天器,该航天器能在电气化轨道上以喷气为动力进行水平发射。航天器的飞行速度将达10马赫,超音速冲压式喷射发动机和机翼将推动它上升到大气层。在此,一个类似于火箭二级推进装置的小型高效载荷设备或太空舱将在飞行器后部点火,并将其送入轨道。航天器最终可飞回并降落到发射地的跑道上。 ...
早期的出舱活动,需要把航天服通过一个“脐带”连接到载人飞船上,获得补给。后来,广泛使用便携式航天服,航天员出舱之后就变身为一个小型的独立“航天器”。载人机动装置的出现,更是“科幻级”地吸引眼球,航天员坐在装置内可通过控制小型发动机,在航天器附近自由飞行。 上述每一次技术迭代,都需要验证。...
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