ЧИСЛОВЕ ВИЗНАЧЕННЯ ПАРАМЕТРІВ АКУСТИЧНИХ ПРОСТОРОВИХ КОЛИВАНЬ ГАЗУ В КАМЕРІ ЗГОРЯННЯ ЕНЕРГЕТИЧНОЇ УСТАНОВКИ НА РІДКОМУ ПАЛИВІ
Published in Aerospace technic and technology • Sep 3, 2026
Authors:,,
O.D. Nikolayev
I.D. Bashliy
Roman Marchan
Abstract
Modern space liquid launch vehicles that launch payload into orbit with lower environmental impact require the use of inexpensive, safe, and reliable propulsion systems. To meet these criteria as much as possible, the design of modern rocket engines is based on the use of advanced elements, material...
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