Development and analysis of simulation of liquid-propellant rocket engine pump head curve obtaining process

Authors

  • Dmitriy Aleksandrovich Savchin Reshetnev Siberian State University of Science and Technology, Russia, Krasnoyarsk
  • Vladimir Pavlovich Nazarov Reshetnev Siberian State University of Science and Technology, Russia, Krasnoyarsk

DOI:

https://doi.org/10.25206/2588-0373-2021-5-1-95-100

Keywords:

automatization, hydraulic test, head curve, piezo-resistive pressure sensor, mathematical model, centrifugal pump

Abstract

The paper describes the model of the centrifugal pump head curve obtaining process which helps in consideration of the implementation of automated systems in liquid-propellant rocket engine manufacturing. The work contains the simulation of automated and non-automated head curve obtaining. The developed model shows that the automated process exceeds the non-automated analog in terms of error values and labor intensity.

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Author Biographies

Dmitriy Aleksandrovich Savchin, Reshetnev Siberian State University of Science and Technology, Russia, Krasnoyarsk

Graduate Student of Aircraft Engines Department.

Vladimir Pavlovich Nazarov, Reshetnev Siberian State University of Science and Technology, Russia, Krasnoyarsk

Candidate of Technical Sciences, Head of Aircraft Engines Department.

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Abstract views: 20

Published

2021-03-31

How to Cite

Savchin Д. А., & Nazarov В. П. (2021). Development and analysis of simulation of liquid-propellant rocket engine pump head curve obtaining process. Omsk Scientific Bulletin. Series «Aviation-Rocket and Power Engineering», 5(1), 95–100. https://doi.org/10.25206/2588-0373-2021-5-1-95-100

Issue

Section

Aviation and rocket-space engineering