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首页> 外文期刊>International journal of hydrogen energy >Review of engineering solutions applicable in tests of liquid rocket engines and propulsion systems employing hydrogen as a fuel and relevant safety assurance aspects
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Review of engineering solutions applicable in tests of liquid rocket engines and propulsion systems employing hydrogen as a fuel and relevant safety assurance aspects

机译：审查适用于以氢为燃料的液体火箭发动机和推进系统测试的工程解决方案以及相关的安全保证方面

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The review presents the author's papers on specific features of experimental development of oxygen-hydrogen liquid rocket engines (LRE), namely the 11D56, 11D57, RD0120, KVD1, and a number of propulsion units and power plants, as well as compares some data on propulsion development activities with relevant data obtained abroad. Also has been shown a role of model studies, component-level tests of engine units and systems, including those performed at simulated flight conditions, and integrated tests in support of experimental development of advanced engines and propulsion systems designed for rocket upper stages. There have been considered techniques and equipment intended to ensure safety of ground testing of rocket engines and power plants involving the use of effective diagnostic systems and emergency protection systems. (C) 2017 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.
机译：这篇综述介绍了作者关于11D56、11D57，RD0120，KVD1以及氢氧液体火箭发动机（LRE）实验开发的特定特征的论文，并比较了一些数据。推进发展活动，并从国外获得相关数据。还显示了模型研究，发动机单元和系统的组件级测试（包括在模拟飞行条件下进行的测试）以及支持用于火箭高级设计的先进发动机和推进系统的实验开发的综合测试的作用。已经考虑了旨在确保火箭发动机和发电厂的地面测试安全的技术和设备，包括使用有效的诊断系统和应急保护系统。 （C）2017氢能出版物有限公司。由Elsevier Ltd.出版。保留所有权利。

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