航天系统. 立方体卫星(CubeSats

[中文适用范围]： 本文档涉及 CubeSats、CubeSat Deployer 以及保证/质量术语和指标的相关验证。 本文件定义了一类独特的皮卫星，即立方体卫星。 立方体卫星是世界各地大学空间开发项目的理想选择。 除了在教育太空科学家和工程师方面发挥重要作用外，立方体卫星还为下一代太空小型有效载荷的测试和空间鉴定提供了一个低成本平台。 该项目的一个关键组成部分是标准 CubeSat Deployer 的开发。 该部署器能够释放大量立方体卫星作为各种发射器上的辅助有效载荷。 标准Deployer要求所有CubeSat符合共同的物理要求，并共享标准Deployer接口。 通过开发大量航天器共享的标准，可以显着减少立方体卫星的开发时间和成本。 CubeSat 设计、鉴定和验收测试的规范控制通常采用其他小型卫星特定标准，但 CubeSat/Deployer 发射环境测试除外。 [外文原描述]： 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 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.