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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, 2017-10-24 - 2017-10-26, Glasgow, United Kingdom UK.

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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 AuthorsAuthor's ORCID iDORCID Put Code
Weuta, PeterUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Ortelt, MarkusUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hofmann, ThoralfUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
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 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 Start Date:24 October 2017
Event End Date:26 October 2017
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 12:23
Last Modified:28 May 2025 13:19

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