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Combustion dynamics in cryogenic rocket engines: Research programme at DLR Lampoldshausen

Hardi, Justin and Traudt, Tobias and Bombardieri, Cristiano and Börner, Michael and Beinke, Scott and Armbruster, Wolfgang and Blanco, Nicolas and Tonti, Federica and Suslov, Dmitry and Dally, Bassam and Oschwald, Michael (2018) Combustion dynamics in cryogenic rocket engines: Research programme at DLR Lampoldshausen. Acta Astronautica, 147, pp. 251-258. Elsevier. doi: 10.1016/j.actaastro.2018.04.002. ISSN 0094-5765.

Full text not available from this repository.

Official URL: https://www.sciencedirect.com/science/article/abs/pii/S0094576517318155

Abstract

The Combustion Dynamics group in the Rocket Propulsion Department at the German Aerospace Center (DLR), Lampoldshausen, strives to advance the understanding of dynamic processes in cryogenic rocket engines. Leveraging the test facilities and experimental expertise at DLR Lampoldshausen, the group has taken a primarily experimental approach to investigating transient flows, ignition, and combustion instabilities for over one and a half decades. This article provides a summary of recent achievements, and an overview of current and planned research activities.

Item URL in elib:https://elib.dlr.de/131462/
Document Type:Article
Title:Combustion dynamics in cryogenic rocket engines: Research programme at DLR Lampoldshausen
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Hardi, JustinJustin.Hardi (at) dlr.dehttps://orcid.org/0000-0003-3258-5261
Traudt, TobiasTobias.Traudt (at) dlr.deUNSPECIFIED
Bombardieri, CristianoInstitute of Space Propulsion, DLR Lampoldshausen, GermanyUNSPECIFIED
Börner, MichaelMichael.Boerner (at) dlr.dehttps://orcid.org/0000-0002-3441-2869
Beinke, ScottInstitute of Space Propulsion, DLR Lampoldshausen, GermanyUNSPECIFIED
Armbruster, WolfgangWolfgang.Armbruster (at) dlr.dehttps://orcid.org/0000-0002-4859-4173
Blanco, NicolasInstitute of Space Propulsion, DLR Lampoldshausen, GermanyUNSPECIFIED
Tonti, FedericaFederica.Tonti (at) dlr.dehttps://orcid.org/0000-0002-2797-349X
Suslov, DmitryDmitry.Suslov (at) dlr.dehttps://orcid.org/0000-0002-5160-9292
Dally, BassamSchool of Mechanical Eng., Univ. of Adelaide, AustraliaUNSPECIFIED
Oschwald, MichaelMichael.Oschwald (at) dlr.dehttps://orcid.org/0000-0002-9579-9825
Date:2018
Journal or Publication Title:Acta Astronautica
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:147
DOI :10.1016/j.actaastro.2018.04.002
Page Range:pp. 251-258
Publisher:Elsevier
ISSN:0094-5765
Status:Published
Keywords:Liquid propellant rocket engines, Cryogenic propellants, Transients, Ignition, Combustion instability
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Antriebsystemtechnik - Schubkammertechnologie (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:20 Dec 2019 08:50
Last Modified:20 Dec 2019 08:50

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