Space systems — Spacecraft-to-launch-vehicle interface control document
空间系统——航天器与运载火箭接口控制文件
发布日期:
2003-10-30
ISO 15863:2003的目的是为航天器(SC)和运载火箭(LV)组织提供提交接口控制文件(ICD)的通用格式,以验证和控制专用任务的SC和LV之间的兼容性。ISO 15863:2003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到发射场接口有关的所有机械、电气、射频和电磁方面、感应环境的验证分析和测试,以及发射场操作所需的设施和支持。
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.