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ADVANCEMENT OF ROCKET ENGINE PERFORMANCE THROUGH NOVEL APPROACHES FOR THRUST CHAMBER DESIGN

Ortelt, Markus and Hald, Hermann and Michaelides, Stelios and Seiler, Helge and Herdrich, Georg (2017) ADVANCEMENT OF ROCKET ENGINE PERFORMANCE THROUGH NOVEL APPROACHES FOR THRUST CHAMBER DESIGN. 68th International Astronautical Congress, Australia, 2017-09-25 - 2017-09-29, Adelaide, Australien.

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Item URL in elib:https://elib.dlr.de/116522/
Document Type:Conference or Workshop Item (Speech)
Title:ADVANCEMENT OF ROCKET ENGINE PERFORMANCE THROUGH NOVEL APPROACHES FOR THRUST CHAMBER DESIGN
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Ortelt, MarkusUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hald, HermannUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Michaelides, SteliosUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Seiler, HelgeUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Herdrich, GeorgUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2017
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Keramische Raketenbrennkammer, Raketen-Injektor, Additive Layer Manufacturing ALM, Transpiration cooled rocket thrust chamber, rocket thrust chamber, rocket injector
Event Title:68th International Astronautical Congress, Australia
Event Location:Adelaide, Australien
Event Type:international Conference
Event Start Date:25 September 2017
Event End Date:29 September 2017
Organizer:International Astronautical Federation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space System Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Space System Technology
DLR - Research theme (Project):Proj Selec ALS Druckverfahren (old)
Location: Stuttgart
Institutes and Institutions:Institute of Structures and Design > Space System Integration
Deposited By: Ortelt, Markus
Deposited On:11 Dec 2017 12:24
Last Modified:28 May 2025 13:12

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