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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Hald, H.	BK	UNSPECIFIED	UNSPECIFIED
Ortelt, M.	BK	UNSPECIFIED	UNSPECIFIED
Fischer, I.	BK	UNSPECIFIED	UNSPECIFIED
Greuel, D.	RA	UNSPECIFIED	UNSPECIFIED

Date:

2003

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

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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