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Preliminary Design of a Hybrid Propulsion Mini Launcher

De Pace, Andrea (2019) Preliminary Design of a Hybrid Propulsion Mini Launcher. Master's, Politecnico di Torino.

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Item URL in elib:https://elib.dlr.de/132948/
Document Type:Thesis (Master's)
Title:Preliminary Design of a Hybrid Propulsion Mini Launcher
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
De Pace, AndreaGerman Aeorspace Center DLR, Inst. of Space Propulsion, Lampoldshausen, DUNSPECIFIEDUNSPECIFIED
Refereed publication:No
Open Access:No
Keywords:hybrid rocket engine
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 - Antriebsystemtechnik - Schubkammertechnologie (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Propellants
Deposited By: Hanke, Michaela
Deposited On:18 Dec 2019 16:06
Last Modified:18 Dec 2019 16:06

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