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Structures for propulsion system: design and analysis of a hybrid rocket’s combustion chamber

Siotto, Federica (2020) Structures for propulsion system: design and analysis of a hybrid rocket’s combustion chamber. Master's, Politecnico di Torino.

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Item URL in elib:https://elib.dlr.de/138521/
Document Type:Thesis (Master's)
Title:Structures for propulsion system: design and analysis of a hybrid rocket’s combustion chamber
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Siotto, FedericaUNSPECIFIEDUNSPECIFIED
Date:2020
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:130
Status:Published
Keywords:combustion chamber, CFRP, pressure vessel
Institution:Politecnico di Torino
Department:Dipartimento di Ingegneria Meccanica e Aerospaziale
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Reusable Space Systems and Propulsion Technology
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Leitungsbereich RA
Deposited By: Hanke, Michaela
Deposited On:30 Nov 2020 08:17
Last Modified:30 Nov 2020 08:17

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