Increasing efficiency of pressurization of the rocket tanks in the flight

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Abstract

The analysis of the onboard rocket tanks pressurization system functioning is presented. The basic direction of the rocket tanks pressurization process are proposed.

About the authors

V. V. Biryuk

Samara State Aerospace University

Author for correspondence.
Email: vest@ssau.ru
Russian Federation

V. A. Kapitonov

State Research and Production Space Rocket Center «TsSKB-Progress»

Email: vest@ssau.ru
Russian Federation

A. V. Smorodin

State Research and Production Space Rocket Center «TsSKB-Progress»

Email: vest@ssau.ru
Russian Federation

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Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

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