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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, 25.-29. Sep. 2017, Adelaide, Australien. (In Press)

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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 AuthorsAuthors ORCID iD
Ortelt, MarkusMarkus.Ortelt (at) dlr.deUNSPECIFIED
Hald, HermannHermann.Hald (at) dlr.deUNSPECIFIED
Michaelides, SteliosStelios.Michaelides (at) dlr.deUNSPECIFIED
Seiler, Helgehelge.seiler (at) dlr.deUNSPECIFIED
Herdrich, Georgherdrich (at) irs.uni-stuttgart.deUNSPECIFIED
Date:2017
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:In Press
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 Dates:25.-29. Sep. 2017
Organizer:International Astronautical Federation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Technik für Raumfahrtsysteme
DLR - Research theme (Project):Proj Selec ALS Druckverfahren
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:31 Jul 2019 20:14

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