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New Techniques and Materials in Cooling for Cryogenic Rocket Engines

Greuel, D. and Suslov, D. and Haidn, O. and Korger, G. and Fritscher, K. (2002) New Techniques and Materials in Cooling for Cryogenic Rocket Engines. In: 4th International Conference on Green Propulsion for Space Propulsion. 4th International Conference on Green Propulsion for Space Propulsion, Noordwijk, The Netherlands, 20-22 June 2002, Noordwijk, The Netherlands.

Full text not available from this repository.

Abstract

Rocket engine design engineers are faced with an ever increasing demand for higher performance and reliability as well as reduced costs. Among the different methods which are proposed in order to increase the life of combustion chamber liners are two techniques which are the most prospective to fulfil these requirements: first, effusion cooled porous carbon-fibre reinforced carbon (C/C) combustion chamber walls and second, thermal barrier coatings (TBC) of standard copper alloy combustion chamber liners using yttria (Y203) stabilized zirconia (ZrO2). Since presently, it is not clear whether one single technology can fulfil all requirements, both methods have to be developed to a state which allows a final decision.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2003,
Title:New Techniques and Materials in Cooling for Cryogenic Rocket Engines
Authors:
AuthorsInstitution or Email of Authors
Greuel, D.UNSPECIFIED
Suslov, D.UNSPECIFIED
Haidn, O.UNSPECIFIED
Korger, G.UNSPECIFIED
Fritscher, K.UNSPECIFIED
Date:2002
Journal or Publication Title:4th International Conference on Green Propulsion for Space Propulsion
Editors:
EditorsEmail
CNES, UNSPECIFIED
Status:Published
Keywords:combustion chamber, liner, effusion cooled
Event Title:4th International Conference on Green Propulsion for Space Propulsion, Noordwijk, The Netherlands, 20-22 June 2002
Event Location:Noordwijk, The Netherlands
Event Type:international Conference
Organizer:Centre National D'Etudes Spatiales (CNES)
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):W - Antriebsystemtechnik - Faserkeramische Brennkammer (old)
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design
Institute of Structures and Design > Space Structural Components
Deposited By: Monika Lohmiller
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 17:48

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