Thermal loading of spent rocket stage structure during ballistic descent

Thermal loading of spent rocket stage structure during ballistic descent

The results of a numerical calculation of the aerodynamic heating of a spent rocket stage structural elements during its controlled descent along a ballistic trajectory are presented. The influence of the initial trajectory parameters on the specific convective and radiant heat fluxes is determine...

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Bibliographic Details
Main Authors: V. Yu. Kudentsov, A. V. Kudentsov, N. A. Kuzina, V. I. Bimatov
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Budgetary Educational Institution of Higher Education 2022-03-01
Series:Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
Subjects:
heat flows
rocket stage
aerodynamic heating
ballistic trajectory
Online Access:https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2022/%D0%A2.%206,%20%E2%84%961%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/101-108%20%D0%9A%D1%83%D0%B4%D0%B5%D0%BD%D1%86%D0%BE%D0%B2%20%D0%92.%20%D0%AE.,%20%D0%9A%D1%83%D0%B4%D0%B5%D0%BD%D1%86%D0%BE%D0%B2%20%D0%90.%20%D0%92.,%20%D0%9A%D1%83%D0%B7%D0%B8%D0%BD%D0%B0%20%D0%9D.%20%D0%90.,%20%D0%91%D0%B8%D0%BC%D0%B0%D1%82%D0%BE%D0%B2%20%D0%92.%D0%98..pdf

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