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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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