空间被动氢激射器氢源设计与实验研究

Wenming Wang, Guohui Shen, Hefei Zheng, Jing Li
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摘要

根据对耗氢率和工作寿命的需求,由离子泵电流的转换和耗氢实验设备的测试计算得到的氢源容量的最小值约为25.4 atm·L,考虑到冗余,实际应等于40 atm·L左右,边际系数为1.6。与高压气体技术储氢相比,相同体积的固体合金储氢使压力降低了近一个数量级。采用金属探伤、膨胀试验和质谱仪检漏等技术,提高了氢源的可靠性。根据氢源泄油平台试验和长寿命评估,建立了氢源数学模型,预测氢源寿命可达12年以上。结果表明,该氢源满足空间被动氢激射器的安全性、可靠性和寿命要求。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design and experimental study of the hydrogen source of space passive hydrogen maser
The minimum value of the hydrogen source capacity, based on the demand for a hydrogen consumption rate and a working life, calculated from the conversion of ion pump current and the test of hydrogen consumption experimental equipment, is about 25.4 atm·L Considering the redundancy, it should be actually equal to about 40 atm·L, and the marginal coefficient amounts to 1.6. Compared with the storage of hydrogen by high-pressure gas technology, the storage by solid alloy in the same volume decreases the pressure by almost one order of magnitude. The reliability of hydrogen source is improved by the technology of metal detection, bulge test and mass spectrometer leak detection. According to the tests of hydrogen source bleed platform and assessment of long lifetime, a mathematical model of hydrogen source is built up, predicting the lifetime of hydrogen source to more than 12 years. The results indicate that the hydrogen source satisfies the requirements for security, reliability and lifetime of the space passive hydrogen maser.
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