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LOX/CH4 Hot Firing Dual Bell Nozzle Testing: Part II - Characteristics of Combustion Instability and Heat Flux -

Takahashi, H. and Tomita, T. and Génin, C. and Schneider, D (2015) LOX/CH4 Hot Firing Dual Bell Nozzle Testing: Part II - Characteristics of Combustion Instability and Heat Flux -. 51st AIAA Joint Propulsion Conference, 27. - 29. Jul. 2015, Orlando, FL, USA. DOI: 10.2514/6.2015-4156

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Item URL in elib:https://elib.dlr.de/99612/
Document Type:Conference or Workshop Item (Speech)
Title:LOX/CH4 Hot Firing Dual Bell Nozzle Testing: Part II - Characteristics of Combustion Instability and Heat Flux -
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Takahashi, H.JAXA, Kakuda, JapanUNSPECIFIED
Tomita, T.JAXA, Kakuda, JapanUNSPECIFIED
Génin, C.Chloe.Genin (at) dlr.deUNSPECIFIED
Schneider, DDirk.Schneider (at) dlr.deUNSPECIFIED
Date:2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2015-4156
Status:Published
Keywords:rocket nozzle, combustion instability
Event Title:51st AIAA Joint Propulsion Conference
Event Location:Orlando, FL, USA
Event Type:international Conference
Event Dates:27. - 29. Jul. 2015
Organizer:AIAA
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 - ProTAU + Prop2020 Hochleistungstriebwerke
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:20 Nov 2015 09:15
Last Modified:10 May 2016 23:35

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