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LOX/CH4 Hot Firing Dual Bell Nozzle Testing: Part I - Transitional Behavior -

Génin, C. and Schneider, Dirk and Tomita, T. and Takahashi, H. (2015) LOX/CH4 Hot Firing Dual Bell Nozzle Testing: Part I - Transitional Behavior -. 51st AIAA Joint Propulsion Conference, 27. - 29. Jul. 2015, Orlando, FL, USA. DOI: 10.2514/6.2015-4155

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/99606/
Document Type:Conference or Workshop Item (Speech)
Title:LOX/CH4 Hot Firing Dual Bell Nozzle Testing: Part I - Transitional Behavior -
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Génin, C.Chloe.Genin (at) dlr.deUNSPECIFIED
Schneider, DirkDirk.Schneider (at) dlr.dehttps://orcid.org/0000-0002-4785-4244
Tomita, T.JAXA Kakuda, JapanUNSPECIFIED
Takahashi, H.JAXA Kakuda, JapanUNSPECIFIED
Date:2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI :10.2514/6.2015-4155
Status:Published
Keywords:Dual Bell Nozzle
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 - Antriebsystemtechnik - Schubkammertechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:20 Nov 2015 09:11
Last Modified:01 Dec 2018 19:51

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