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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.

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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 Authors
Hald, H.BK
Ortelt, M.BK
Fischer, I.BK
Greuel, D.RA
Date:2003
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: elib DLR-Beauftragter
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 13:14

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