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CMC Design Approach for Cryogenic Injector Heads of Rocket Thrust Chambers

Ortelt, Markus and Hald, Hermann and Herbertz, Armin and Rotärmel, Waldemar (2010) CMC Design Approach for Cryogenic Injector Heads of Rocket Thrust Chambers. In: Konferenzbeiträge EUCOMAS. EUCOMAS 2010, 07.-08. Juni 2010, Berlin, Deutschland.

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Item URL in elib:https://elib.dlr.de/67898/
Document Type:Conference or Workshop Item (Speech)
Title:CMC Design Approach for Cryogenic Injector Heads of Rocket Thrust Chambers
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Ortelt, MarkusMarkus.Ortelt (at) dlr.deUNSPECIFIED
Hald, Hermannhermann.hald (at) dlr.deUNSPECIFIED
Herbertz, ArminArmin.Herbertz (at) dlr.deUNSPECIFIED
Rotärmel, Waldemarwaldemar.rotaermel (at) dlr.deUNSPECIFIED
Date:8 June 2010
Journal or Publication Title:Konferenzbeiträge EUCOMAS
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Poröser Einspritzkopf, Raketenbrennkammer, CMC-Injektor, Verbrennungsstabilität, Triebstoffaufbereitung, Zerstäubung, kalte Injektion
Event Title:EUCOMAS 2010
Event Location:Berlin, Deutschland
Event Type:international Conference
Event Dates:07.-08. Juni 2010
Organizer:VDI
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:04 Jan 2011 15:55
Last Modified:31 Jul 2019 19:30

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