新一代运载火箭加注液位地面设备统型设计

Jin Bao1,Xu Zifei1,Xu Xin3,2(1．Shanghai institute of Aerospace System Engineering, Shanghai 201100, China;

摘要:

针对我国新一代运载火箭多型号发展导致加注液位地面设备存在型号专用、互不兼容、研制成本高昂等问题，开展统型设计研究，全面分析各型新一代运载火箭对加注液位测量的共性功能与个性化接口需求，进行顶层架构规划，对不同运载火箭加注液位传感器、变换器及地面处理设备进行梳理，对加注液位地面处理设备硬件、软件、接口进行通用化设计，实现单一硬件平台对多型火箭的兼容保障。仿真与测试表明，统型设备在测量精度、可靠性、元器件国产化率等关键指标上均满足所有目标型号的任务要求。经型号真实发射场加注验证满足使用要求，显著提高了地面设备的通用性与保障效率，对适应高密度发射任务具有重要意义。

Abstract:

In response to the issues of model-specific, incompatible, and high development costs of ground equipment for propellant level measurement caused by the multi-model development of China’s new generation launch vehicles, this study conducts unified design research. A comprehensive analysis of the common functional and personalized interface requirements for propellant level measurement across various new generation launch vehicles is performed. A top-level architecture is planned. The propellant level sensors, transducers, and ground processing equipment for different launch vehicles are systematically reviewed. A generalized design for the hardware, software, and interfaces of the ground processing equipment is implemented, enabling a single hardware platform to support multiple launch vehicle models. Simulations and tests demonstrate that the unified equipment meets the mission requirements of all target models in key indicators such as measurement accuracy, reliability, and the localization rate of components. Validation through actual launch site propellant loading tests confirms that the equipment meets operational requirements, significantly improving the universality and support efficiency of ground equipment, which is of great importance for adapting to high-density launch missions.