Registration Number
0225U000258,
(0121U100691)
, R & D reports
Title
Numerical modeling of aerothermogasdynamic and dynamic processes that follow the operation of rocket and space technology objects
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Проведення досліджень щодо прогнозування параметрів аеротермогазодинамічних процесів та динамічних навантажень на активних ділянках траєкторії ОРКТ і при наземному відпрацюванні їх складових систем
Head
Tymoshenko Valerii I., Доктор фізико-математичних наук
Registration Date
08-01-2025
Organization
Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine
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The purpose of the work is to determine the impact of aerothermogasdynamic and dynamic processes on the functioning of promising objects of rocket and space technology in different operating modes to ensure rapid forecasting of aerodynamic, thermal and dynamic loads which influence them
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Object of Research: Numerical modeling algorithms for determining the parameters of aerothermogasdynamic processes and dynamic loads accompanying the operation of rocket and space technology (RST).
Objective of the Work: Verification of numerical modeling algorithms for aerothermogasdynamic processes to promptly determine aerodynamic, thermal, and dynamic loads on RST under various operational conditions and conduct related research.
Research Methods: Computational methods in gas dynamics, hydraulics, and dynamics.
The numerical modeling algorithms for thermogasdynamic and hydraulic processes, as well as aerodynamic, thermal, and dynamic loads in RST systems, were verified in the following areas:
- supersonic aerodynamics of the launch vehicle (LV), considering air intake devices, wings, stabilization and control mechanisms, and body rotation around its axis;
- hydraulic and thermogasdynamic processes in control jet engines systems with various thrust characteristics using traditional and advanced fuels;
- effects of rarefied jet flows on the external atmosphere of spacecraft and aerodynamic loads on their surfaces;
- dynamic loads on the main stages of LV with active control systems during the active phases of flight trajectories, accounting for dynamic and aerodynamic disturbances.
For each of these four areas, relevant studies were conducted using verified numerical modeling algorithms to solve tasks selected and formulated in the previous stages of the work.
The results obtained in the fourth stage of the work will be used for research in the next stage. This research is a continuation of work on topics carried out at the ITM NASU and the SSAU from 2006 to 2020. The results of the work are intended for use in the rocket and space industry.
Product Description
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Ivanova Halyna O.
Halinskyi Valerii P.
Horbuntsov Viacheslav V.
Zavoloka Oleksandr M.
Knyshenko Yurii V.
Petrushenko Mykola M.
Pecherytsia Larysa L.
Smila Tetiana H.
Tуmoshenko Valerii I.
Shaulska Larysa S.
Shcherbakov Volodymyr I.
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2025-01-08
