Year: 2025
Type: conference-paper
Abstract: The paper presents a new mathematical model describing processes in the pneumatic systems of liquid rocket engines.To determine gas parameters, the specific initial value problem was solved.The developed model can be used in the design of tank pressurization systems for liquid rockets.
Source: Людина і космос.
Author: Vitalii Alieksieienko
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: hybrid
OpenAlex ID: W4411067850