标准摘要
[中文适用范围]： 本国际标准的目的是为航天器 (SC) 和运载火箭 (LV) 组织提供用于呈现接口控制文件 (ICD) 的通用格式，以验证和控制 SC 和运载火箭 (LV) 之间的兼容性以执行专用任务。 该国际标准阐述了任务的定义、SC与低压环境的兼容性，包括与SC到低压和SC发射范围接口相关的所有机械、电气、射频和电磁方面，以及验证分析和测试诱导环境，以及发射场运行所需的设施和支持。 [外文原描述]： The purpose of ISO 15863:2003 is to provide spacecraft (SC) and launch vehicle (LV) organizations with the general format for presenting the interface control document (ICD) that verifies and controls the compatibility between SC and LV for a dedicated mission. ISO 15863:2003 addresses the definition of the mission, the compatibility of the SC with the LV environment, including all mechanical, electrical, radio frequency, and electromagnetic aspects related to SC to LV and SC to launch range interfaces, verification analyses and tests for the induced environment, and the necessary facilities and support for launch range operations.
英文名称Space systems — Spacecraft-to-launch-vehicle interface control document