Systems for assuring safety of static firing tests of oxygen/hydrogen propulsion units
Автор: Galeev Ayvengo Gadyevich, Egorov Fedor Andreevich, Polyakhov Aleksandr Dmitrievich, Potapov Vladimir Timofeevich, Sizyakov Nikolay Petrovich, Sokolovskiy Aleksandr Alekseevich
Журнал: Космическая техника и технологии @ktt-energia
Рубрика: Контроль и испытание летательных аппаратов и их систем
Статья в выпуске: 1 (28), 2020 года.
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Static firing tests of oxygen-hydrogen propulsion units with propellant tank load of up to 2 700 kg of hydrogen are run with special safety precautions and using emergency test protection system covering up to 60% of contingencies. Test on propulsion units with higher hydrogen propellant loads (up to 7 000 kg) require additional safety measures, based on improved effectiveness of the fire and explosion prevention systems, emergency protection, and the coverage ratio for emergency (off-nominal) situations. The key factors for improving off-nominal situations coverage ratio during tests are research into systems for earlier detection of hydrogen leaks and the use of inhibitors with nitrogen as the phlegmatizing agent to prevent explosion of the hydrogen/air (oxygen) mixtures. The paper presents results of studies into systems for early detection of hydrogen leaks and design of monitoring equipment based on fiber optics and microcavity structures that have higher speed of response, selectivity, immunity to noise and reliability.
Propulsion system, safety, emergency protection system, off-nominal situation, hydrogen leak, fiber-optic technology
Короткий адрес: https://sciup.org/143177923
IDR: 143177923 | DOI: 10.33950/spacetech-2308-7625-2020-1-71-84