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Examination of Thermomechanical Fatigue in Panels Representing Rocket Engine Combustion Chamber Geometries

Kringe, Pascal (2025) Examination of Thermomechanical Fatigue in Panels Representing Rocket Engine Combustion Chamber Geometries. DLR-Forschungsbericht. DLR-FB-2025-10. Dissertation. RWTH Aachen. 168 S. doi: 10.57676/js82-f364.

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Item URL in elib:https://elib.dlr.de/213982/
Document Type:Monograph (DLR-Forschungsbericht, Dissertation)
Title:Examination of Thermomechanical Fatigue in Panels Representing Rocket Engine Combustion Chamber Geometries
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Kringe, PascalUNSPECIFIEDhttps://orcid.org/0000-0003-2866-8419UNSPECIFIED
Date:2025
Open Access:Yes
DOI:10.57676/js82-f364
Number of Pages:168
ISSN:1434-8454
Status:Published
Keywords:regeneratively cooled rocket combustion chamber, fatigue life investigation, TMF
Institution:RWTH Aachen
Department:Fakultät für Bauingenieurwesen
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Reusable Space Systems and Propulsion Technology, R - Project AKIRA RLV Key Technologies
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion Technology
Deposited By: Hanke, Michaela
Deposited On:09 May 2025 09:40
Last Modified:09 May 2025 13:04

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