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

Justin S. Hardi, Tobias Traudt, Cristiano Bombardieri, Michael Börner, Scott K. Beinke, Wolfgang Armbruster, P. Nicolas Blanco, Federica Tonti, Dmitry Suslov, Bassam Dally, Michael Oschwald

Research output: Chapter in Book/Report/Conference proceedingConference contribution


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.
Original languageEnglish (US)
Title of host publicationProceedings of the International Astronautical Congress, IAC
PublisherInternational Astronautical Federation, IAF
Number of pages10
ISBN (Print)9781510855373
StatePublished - Jan 1 2017
Externally publishedYes

Bibliographical note

Generated from Scopus record by KAUST IRTS on 2022-09-12


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