The flowing part of turbine ZHRD of the closed circuit analysis
Автор: Kraev M.V., Kaichuk L.N., Kraevа Е.M.
Журнал: Сибирский аэрокосмический журнал @vestnik-sibsau
Рубрика: Авиационная и ракетно-космическая техника
Статья в выпуске: 4 (21), 2008 года.
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The flowing part of the gas turbine of the liquid rocket engine of the closed analysis is executed, the movement trajectory is considered in a biphase gas stream structure of the lonely drop, generated after gas generated the prechamber turbine of the stream.
Carrier rocket, turbine, flowing part, drop, trajectory, failure, turbine pump unit
Короткий адрес: https://sciup.org/148175721
IDR: 148175721
Статья научная
