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CMC rocket combustion chamber with effusion cooling

Hald, H. and Ortelt, M. and Fischer, I. and Greuel, D. (2003) CMC rocket combustion chamber with effusion cooling. 54th International Astronautical Congress, Bremen, 29.9.- 3.10.2003.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/15050/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2004,
Title:CMC rocket combustion chamber with effusion cooling
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hald, H.BKUNSPECIFIED
Ortelt, M.BKUNSPECIFIED
Fischer, I.BKUNSPECIFIED
Greuel, D.RAUNSPECIFIED
Date:2003
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:space transportation systems, STS, reusability, CMC, ceramic matrix composites, cryogenic, combustion, cooling
Event Title:54th International Astronautical Congress, Bremen, 29.9.- 3.10.2003
Organizer:International Astronautical Federation
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):UNSPECIFIED
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design
Institute of Space Propulsion
Deposited By: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 13:14

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