Experimental Investigation of Flame Anchoring Behavior in a LOX/LNG Rocket Combustor
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Bibliographic citation
-
In: 10.3390/aerospace10060542
- Event
-
Veröffentlichung
- (where)
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Aachen
- (who)
-
Universitätsbibliothek der RWTH Aachen
- (when)
-
2023
- Creator
-
Martin, Jan
Börner, Michael
Hardi, Justin
Suslov, Dmitry
Oschwald, Michael
- DOI
-
10.18154/RWTH-2023-07220
- URN
-
urn:nbn:de:101:1-2023072601351830548161
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
25.03.2025, 1:51 PM CET
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Martin, Jan
- Börner, Michael
- Hardi, Justin
- Suslov, Dmitry
- Oschwald, Michael
- Universitätsbibliothek der RWTH Aachen
Time of origin
- 2023
Other Objects (12)
Flame dynamics of an injection element operated with LOX/H2, LOX/CNG and LOX/LNG in a sub- and supercritical rocket combustor with large optical access
Flame Characteristics and Response of a High-Pressure LOX/CNG Rocket Combustor with Large Optical Access
Injector-coupled thermoacoustic instabilities in an experimental LOX-methane rocket combustor during start-up
Stockelbusch (lng.)
Bremgarten: LOX Anlagenwerkstatt
Lox. Toni-Apéritif
Cojump Anchoring
Anchoring systems
Cojump anchoring
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Steinhoff, (Dipl. lng.), Kyffhäusertechnikum
Emerging Asia LNG demand
Flame dynamics of an injection element operated with LOX/H2, LOX/CNG and LOX/LNG in a sub- and supercritical rocket combustor with large optical access
Flame Characteristics and Response of a High-Pressure LOX/CNG Rocket Combustor with Large Optical Access
Injector-coupled thermoacoustic instabilities in an experimental LOX-methane rocket combustor during start-up
Stockelbusch (lng.)
Bremgarten: LOX Anlagenwerkstatt
Lox. Toni-Apéritif
Cojump Anchoring
Anchoring systems
Cojump anchoring
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Steinhoff, (Dipl. lng.), Kyffhäusertechnikum
Emerging Asia LNG demand
Flame dynamics of an injection element operated with LOX/H2, LOX/CNG and LOX/LNG in a sub- and supercritical rocket combustor with large optical access
Flame Characteristics and Response of a High-Pressure LOX/CNG Rocket Combustor with Large Optical Access
Injector-coupled thermoacoustic instabilities in an experimental LOX-methane rocket combustor during start-up
Stockelbusch (lng.)
Bremgarten: LOX Anlagenwerkstatt
Lox. Toni-Apéritif
Cojump Anchoring
Anchoring systems
Cojump anchoring
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Steinhoff, (Dipl. lng.), Kyffhäusertechnikum