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Aerothermal Analysis of Reusable First Stage Launcher during Re-Entry Retro-Propulsion

Zilker, Franziska and Ecker, Tobias and Dumont, Etienne and Hannemann, Klaus (2017) Aerothermal Analysis of Reusable First Stage Launcher during Re-Entry Retro-Propulsion. 18. STAB-Workshop 2017, 07.-08. Nov. 2017, Göttingen, Deutschland.

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Item URL in elib:https://elib.dlr.de/115671/
Document Type:Conference or Workshop Item (Speech)
Additional Information:http://www.dlr.de/as/desktopdefault.aspx/tabid-652/1104_read-1678/
Title:Aerothermal Analysis of Reusable First Stage Launcher during Re-Entry Retro-Propulsion
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Zilker, FranziskaUNSPECIFIEDUNSPECIFIED
Ecker, TobiasTobias.Ecker (at) dlr.dehttps://orcid.org/0000-0001-7134-1185
Dumont, EtienneEtienne.Dumont (at) dlr.dehttps://orcid.org/0000-0003-4618-0572
Hannemann, Klausklaus.hannemann (at) dlr.deUNSPECIFIED
Date:2017
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Retropropulsion, wiederverwendbar, erste Stufe, Wiedereintritt, Wärmelasten
Event Title:18. STAB-Workshop 2017
Event Location:Göttingen, Deutschland
Event Type:Workshop
Event Dates:07.-08. Nov. 2017
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation
Location: Bremen , Göttingen
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Bachmann, Barbara
Deposited On:21 Nov 2017 11:11
Last Modified:21 Nov 2017 11:11

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