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Development of reusable liquid Propulsion Units based on transpiration cooled, ceramic thrust Chambers and turbopumps for Launch and in space applications

Weuta, Peter and Ortelt, Markus and Hofmann, Thoralf (2017) Development of reusable liquid Propulsion Units based on transpiration cooled, ceramic thrust Chambers and turbopumps for Launch and in space applications. 15th Reinventing Space Conference, 24.-26. Okt. 2017, Glasgow, United Kingdom UK. (In Press)

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Item URL in elib:https://elib.dlr.de/116517/
Document Type:Conference or Workshop Item (Speech)
Title:Development of reusable liquid Propulsion Units based on transpiration cooled, ceramic thrust Chambers and turbopumps for Launch and in space applications
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Weuta, Peterpeter.weuta (at) wepa-technologies.deUNSPECIFIED
Ortelt, MarkusMarkus.Ortelt (at) dlr.deUNSPECIFIED
Hofmann, Thoralfthoralf.hofmann (at) wepa-technologies.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 bzw. -schubkammer, Ceramic Rocket Thrust Chamber, Transpiration Cooling, Raketen-Turbopumpen, Turbopump, Rocket Injector,
Event Title:15th Reinventing Space Conference
Event Location:Glasgow, United Kingdom UK
Event Type:international Conference
Event Dates:24.-26. Okt. 2017
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 12:23
Last Modified:31 Jul 2019 20:14

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