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基于电化学加速的单推-3推进剂贮箱长贮分析OA

Analysis on long-term storage of DT-3 propellant tank accelerated by electrochemistry

中文摘要英文摘要

提出了融合电化学加速试验与贮箱长贮试验的综合评估方法,结合扫描电镜(Scanning electron microscopy,SEM)、电感耦合等离子光谱(Inductively coupled plasma optical emission spec-trometry,ICP)分析手 段,实现了某液体姿轨控系统长期贮存寿命的高效评估.结果表明:1050A-LF6 电偶对在单推-3 推进剂中无明显的电偶腐蚀效应;采用500 倍加速因子可将产品寿命指标评估周期缩短至16 d,1050A、LF6 等金属材料在单推-3 推进剂的电化学加速贮存过程中,材料与推进剂具有良好的相容性,满足长贮要求;单推-3 推进剂贮箱在40℃贮存360 d 过程中,贮箱推进剂各项技术指标的变化随贮存时间的延长符合饱和型动力学模型趋势,贮存至360 d 推进剂仍符合国军标使用指标要求.建立的试验方法为液体姿控推进剂贮箱寿命管理研究提供了新的技术途径.

A comprehensive evaluation method combining electrochemical accelerated tests and long-term storage tests of storage tanks was proposed.By utilizing scanning electron microscopy(SEM)and inductively coupled plasma optical emission spectrometry(ICP)analysis techniques,an efficient evaluation of the long-term storage life of a liquid propulsion system for attitude and orbit control was achieved.The research shows that the 1050A-LF6 electrochemical couple pair has no obvious galvanic corrosion effect in the DT-3 monopropellant.The evaluation cycle of product life indicators can be shortened to 16 days by adopting a 500 times acceleration factor.During the electrochemical accelerated storage process of DT-3 monopropellant,the 1050A and LF6 metal materials have good compatibility with the propellant,meeting the requirements of long-term storage.During the 360 days storage of the DT-3 monopropellant pressurized storage tank at 40℃,the changes in the technical indicators of the tank propellant with the extension of storage time follow a trend of the saturation kinetic model,and the propellant still meets the usage index requirements of the national military standard after 360 days of storage.The test system method provides a new technical approach for the study on the life management of liquid attitude control propellant tanks.

龚全鑫;刘嘉兴;唐占梅;王新新

上海空间推进研究所,上海 201112上海空间推进研究所,上海 201112北京航天试验技术研究所,北京 100074上海空间推进研究所,上海 201112

航空航天

单推-3推进剂贮存寿命电化学加速动力学模型

DT-3 monopropellantstorage lifeelectrochemical accelerationkinetic model

《火箭推进》 2026 (2)

75-84,10

10.3969/j.issn.1672-9374.2026.02.008

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