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GH2/GO2 Supply Facility for Hot Plume Testing in the Vertical Test Section Cologne (VMK)

Kirchheck, Daniel and Gülhan, Ali (2016) GH2/GO2 Supply Facility for Hot Plume Testing in the Vertical Test Section Cologne (VMK). Project Report. Technische Universität München. 8 S.

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Official URL: http://www.sfbtr40.de/?id=68


The paper belongs to a series of investigations of hot plume interaction phenomena in the field of space transportation. Scientific motivation of these investigations is the understanding of the physical mechanisms in base flows that are for example present at rocket launchers. The paper shortly summarizes the technical challenges that are resulting from base flow interaction phenomena and develops a motivation for an enhancement of the experimental testing capabilities in that field. In the second part, an effort of the German Aerospace Center (DLR) to achieve that goal by expanding the vertical wind tunnel facility in Cologne by a gaseous hydrogen oxygen supply unit to enable hot plume interaction testing with GH2/GO2 combustion is presented. The design of the facility is summarized and an outlook on the gain for future investigations in that field is given in the conclusions.

Item URL in elib:https://elib.dlr.de/114008/
Document Type:Monograph (Project Report)
Title:GH2/GO2 Supply Facility for Hot Plume Testing in the Vertical Test Section Cologne (VMK)
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Refereed publication:No
Open Access:No
Number of Pages:8
Keywords:rocket base flow, plume interaction, rocket plume Simulation, hot plume testing facility
Institution:Technische Universität München
Department:Lehrstuhl für Aerodynamik
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 - Raumfahrzeugsysteme - Anlagen u. Messtechnik (old)
Location: Köln-Porz
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology
Deposited By: Kirchheck, Daniel
Deposited On:18 Sep 2017 14:07
Last Modified:18 Sep 2017 14:07

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