本文件规定了绕地球运动空间物体轨道确定和预报中的主要力模型、输入输出和技术流程。
本文件适用于在自然力作用下绕地球运动空间物体测量、编目和预警中涉及的空间物体轨道数据生成、轨道运动状态预测及其应用。
This standard specifies terms and definitions of launch vehicle (LV) in aspects of universal purpose, systems, trajectory, loads and dynamic characteristics, aerodynamics, aerodynamic heating, mechanical environment, thermal environment, electromagnetic environment, natural environment, structure system, separation system, engine, pressurization and feeding system, control system, measurement system, propellant utilization system, failure detection and processing system, escape system, power supply and distribution system, ground test-launch-control system, launch site and integration assembly, and test and launch process flow.
This standard is applicable to LV development, including design, manufacture, test and launch, etc.
This standard specifies the basic requirements for the measurement of the spacecraft flight environments generated by the launch vehicle,telemetry data processing and formats of analysis reports.
This standard is applicable to the interface of launch-vehicle-to-spacecraft(SC/LV)flight environment telemetry data processing and analysis.