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Investigation of the combustion process in hybrid rocket engines with energetic additives with a water-cooled sampling probe system

Carissimi, Juri (2012) Investigation of the combustion process in hybrid rocket engines with energetic additives with a water-cooled sampling probe system. Master's, Politecnico Milano, Italy.

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Item URL in elib:https://elib.dlr.de/81295/
Document Type:Thesis (Master's)
Title:Investigation of the combustion process in hybrid rocket engines with energetic additives with a water-cooled sampling probe system
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Carissimi, JuriUNSPECIFIEDUNSPECIFIED
Date:2012
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:rocket propulsion, rocket engine
Institution:Politecnico Milano, Italy
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 > Propellants
Deposited By: Hanke, Michaela
Deposited On:21 Feb 2013 10:48
Last Modified:21 Feb 2013 10:48

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