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Stationary and Dynamic Thermal Analyses of Cryogenic Liquid Rocket Combustion Chamber Walls

Riccius, J. and Zametaev, E. (2002) Stationary and Dynamic Thermal Analyses of Cryogenic Liquid Rocket Combustion Chamber Walls. In: AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, pp. 1-11. AIAA. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, July 07-10, 2002.

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Abstract

A comparative study of stationary and dynamic thermal analyses of a typical rocket combustion chamber wall during a full cycle including pre cooling, hot run, post cooling, relaxation is presented. Furthermore, the influence of the different thermal fields on the following analyses are shown: 1. Nonlinear structural analysis of the combustion chamber wall with cyclic thermal and mechanical loading 2. Post processing life time estimation of the combustion chamber wall

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2002, monograph_id=AIAA 2002-3694,
Title:Stationary and Dynamic Thermal Analyses of Cryogenic Liquid Rocket Combustion Chamber Walls
Authors:
AuthorsInstitution or Email of Authors
Riccius, J.UNSPECIFIED
Zametaev, E.UNSPECIFIED
Date:2002
Journal or Publication Title:AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Page Range:pp. 1-11
Editors:
EditorsEmail
American Institute of Aeronautics and Astronautics, UNSPECIFIED
Publisher:AIAA
Status:Published
Event Title:38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, July 07-10, 2002
Organizer:American Institute of Aeronautics and Astronautics
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):E -- no assignement
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Monika Lohmiller
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:58

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