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Towards an Optimal Concept for Numerical Codes Simulating Thrust Chamber Processes in High Pressure Chemical Propulsion Systems

Schley, C.-A. and Hagemann, G. and Krülle, G. (1995) Towards an Optimal Concept for Numerical Codes Simulating Thrust Chamber Processes in High Pressure Chemical Propulsion Systems. In: IAF. 46th Intern. Astronautical Federation Congress (IAF), Oct. 2-6, 1995, Oslo, Norway.

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Document Type:Conference or Workshop Item (Paper)
Additional Information: institution=IAF, LIDO-Berichtsjahr=1995,
Title:Towards an Optimal Concept for Numerical Codes Simulating Thrust Chamber Processes in High Pressure Chemical Propulsion Systems
Authors:
AuthorsInstitution or Email of Authors
Schley, C.-A.UNSPECIFIED
Hagemann, G.UNSPECIFIED
Krülle, G.UNSPECIFIED
Date:1995
Journal or Publication Title:IAF
Series Name:IAF-95-S.1.04
Status:Published
Keywords:Rocket Engine, Hardware Problem Areas, Numerical Modelling, Solver, Boundary Conditions, Grid Generation, Physical Models
Event Title:46th Intern. Astronautical Federation Congress (IAF), Oct. 2-6, 1995, Oslo, Norway
HGF - Research field:UNSPECIFIED
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:UNSPECIFIED
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):E -- no assignement
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:37

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