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Design of an advanced, sub-scale, optical accessible research rocket combustor for the investigation of high-pressure cryogenic combustion

Park, Jaehong (2017) Design of an advanced, sub-scale, optical accessible research rocket combustor for the investigation of high-pressure cryogenic combustion. Master's. DLR-Interner Bericht. DLR-IB-RA-LA-2017-304, 137 S.

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Item URL in elib:https://elib.dlr.de/118096/
Document Type:Monograph (DLR-Interner Bericht, Master's)
Title:Design of an advanced, sub-scale, optical accessible research rocket combustor for the investigation of high-pressure cryogenic combustion
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Park, JaehongInstitut für Raumfahrtantriebe, DLR Lampoldshausen, DUNSPECIFIED
Date:2017
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:137
Status:Published
Keywords:rocket combustor, cryogenic
Institution:TU Berlin
Department:Department of Aeronautics and Astronautics - Chair of Space Technology
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:10 Jan 2018 14:28
Last Modified:04 Apr 2018 08:28

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