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COMPARISON OF OXYGEN-HYDROGEN COMBUSTION VISUALISION TECHNIQUES UNDER REPRESENTATIVE CONDITIONS

Webster, Samuel and Hardi, Justin and Oschwald, Michael (2016) COMPARISON OF OXYGEN-HYDROGEN COMBUSTION VISUALISION TECHNIQUES UNDER REPRESENTATIVE CONDITIONS. In: Proceedings. Space Propulsion 2016, 2. - 6. May 2016, Rome, Italy.

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Item URL in elib:https://elib.dlr.de/107822/
Document Type:Conference or Workshop Item (Speech)
Title:COMPARISON OF OXYGEN-HYDROGEN COMBUSTION VISUALISION TECHNIQUES UNDER REPRESENTATIVE CONDITIONS
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Webster, SamuelInstitut für Raumfahrtantriebe, DLR LampoldshausenUNSPECIFIED
Hardi, JustinJustin.Hardi (at) dlr.deUNSPECIFIED
Oschwald, MichaelMichael.Oschwald (at) dlr.deUNSPECIFIED
Date:2016
Journal or Publication Title:Proceedings
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:liquid propellant rocket engine, combustion instability, optical diagnostics, flame visualisation, cryogenic propellants
Event Title:Space Propulsion 2016
Event Location:Rome, Italy
Event Type:international Conference
Event Dates:2. - 6. May 2016
Organizer:3AF
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:16 Nov 2016 07:56
Last Modified:31 Jul 2019 20:05

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