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Thermomechanische Analyse einer koaxial segmentierten Injektorkopf-Hybridstruktur für kryogene Raketenantriebe

Rotärmel, Waldemar (2006) Thermomechanische Analyse einer koaxial segmentierten Injektorkopf-Hybridstruktur für kryogene Raketenantriebe. Diploma. DLR-Interner Bericht. IB 435-2006/57, 84 S.

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Item URL in elib:https://elib.dlr.de/46257/
Document Type:Monograph (DLR-Interner Bericht, Diploma)
Title:Thermomechanische Analyse einer koaxial segmentierten Injektorkopf-Hybridstruktur für kryogene Raketenantriebe
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Rotärmel, WaldemarUNSPECIFIEDUNSPECIFIED
Date:2006
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:84
Status:Published
Keywords:Raketeneinspritzkopf, Faserkeramik, Hybridstruktur, Poröser Injektor, Injektor für kryogene Raketenbrennkammern
Institution:Universität Stuttgart
Department:Luft- und Raumfahrttechnik
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 > Space Structural Components
Deposited By: Ortelt, Markus
Deposited On:28 Dec 2006
Last Modified:27 Apr 2009 13:20

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