MODELING OF GAS FLOW IN PNEUMATIC SYSTEMS OF LRE BASED ON LOCAL MODELS OF SYSTEM ELEMENTS
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.
Authors
- Vitalii Alieksieienko
Institutions
- Dnipro University of Technology (UA)
Publication Details
- Journal
- Людина і космос.
- Published
- 2025-04-18
- DOI
- https://doi.org/10.62717/2221-4550-2025-1-070
- Primary Topic
- Mechanical and Thermal Properties Analysis
- Type
- article
- Field-Weighted Citation Impact
- 0.00