Инновационная модель применения жидкого азота для охлаждения ракетного топлива…
ISSN 0236-3941. Вестник МГТУ им. Н.Э. Баумана. Сер. Машиностроение. 2017. № 3
15
dependences and the results of rocket fuel cooling analy-
sis. Moreover, we evaluated the model effectiveness.
Findings of the research show that the proposed model
allows reducing the cost of liquid nitrogen for rocket fuel
cooling in comparison with the existing cooling system at
the launch complex "Soyuz" by 40 %. According to the
estimates, the materials consumption is also reduced by
4.5 times. The innovative model we developed can signi-
ficantly simplify the design and operational calculations
of rocket fuel cooling processes, which is supported by
the results of numerical calculations
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