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Analysis and Preliminary Design of a Hybrid Propulsion Lunar Lander

Schmierer, C. and Tomilin, K. and Kobald, Mario and Steelant, Johan and Schlechtriem, S. (2016) Analysis and Preliminary Design of a Hybrid Propulsion Lunar Lander. Space Propulsion 2016, 02.-06. Mai 2016, Rom, Italien.

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Item URL in elib:https://elib.dlr.de/105038/
Document Type:Conference or Workshop Item (Speech)
Title:Analysis and Preliminary Design of a Hybrid Propulsion Lunar Lander
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schmierer, C.christian.schmierer (at) dlr.deUNSPECIFIED
Tomilin, K.konstantin.tomilin (at) dlr.deUNSPECIFIED
Kobald, MarioMario.Kobald (at) dlr.dehttps://orcid.org/0000-0002-1708-3944
Steelant, JohanESA-ESTEC, NLUNSPECIFIED
Schlechtriem, S.Stefan.Schlechtriem (at) dlr.deUNSPECIFIED
Date:2 May 2016
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Hybrid rocket Propulsion, lunar lander, H2O2, LOX, Paraffin fuel
Event Title:Space Propulsion 2016
Event Location:Rom, Italien
Event Type:international Conference
Event Dates:02.-06. Mai 2016
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Antriebsystemtechnik - Raketenantriebtests
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Propellants
Deposited By: Kobald, Dr. Mario
Deposited On:04 Jul 2016 09:48
Last Modified:01 Dec 2018 19:52

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