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Numerical simulation of a sub-scale rocket combustor, carried out in the framework of CNES-DLR cooperation

Di Fabbio, Tony (2019) Numerical simulation of a sub-scale rocket combustor, carried out in the framework of CNES-DLR cooperation. Master's, Politecnico di Torino, Italy.

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Item URL in elib:https://elib.dlr.de/132947/
Document Type:Thesis (Master's)
Title:Numerical simulation of a sub-scale rocket combustor, carried out in the framework of CNES-DLR cooperation
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Di Fabbio, TonyDLR, Inst. für Raumfahrtantriebe, Lampoldshausen, DUNSPECIFIED
Date:2019
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:134
Status:Published
Keywords:rocket combustor
Institution:Politecnico di Torino, Italy
Department:DIPARTIMENTO DI INGEGNERIA MECCANICA E AEROSPAZIALE
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 - Schubkammertechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:18 Dec 2019 16:05
Last Modified:18 Dec 2019 16:05

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