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Experimental Determination of Recombination Coefficients at High Pressures

Esser, Burkard and Gülhan, Ali and Koch, Uwe (2015) Experimental Determination of Recombination Coefficients at High Pressures. 8th European Symposium on Aerothermodynamics for Space Vehicles, 02. - 06. März 2015, Lissabon, Portugal.

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Abstract

In the arc-heated facility L2K, an experimental campaign was performed which aimed at the determination of recombination coefficients at conditions with high stagnation pressure which are of particular interest for re-entry from LEO. Tests were performed on two TPS materials with a variation of surface temperature, stagnation pressure, and atmosphere. During a preparatory campaign suitable operating conditions and facility configurations were determined for all 24 test cases. Based on the measured data, details of the flow conditions could be identified. These data were used to evaluated recombination coefficients according to Goulard’s method. Due to the low dissociation rates at the higher stagnation pressures, the evaluation was successful for the lowest stagnation pressure level of 2000 Pa mainly. In nitrogen flow, results were obtained for the high temperature cases only.

Item URL in elib:https://elib.dlr.de/97922/
Document Type:Conference or Workshop Item (Speech)
Title:Experimental Determination of Recombination Coefficients at High Pressures
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Esser, BurkardUNSPECIFIEDUNSPECIFIED
Gülhan, AliUNSPECIFIEDUNSPECIFIED
Koch, UweUNSPECIFIEDUNSPECIFIED
Date:2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-8
Series Name:Conference Proceedings online
Status:Published
Keywords:Heat flux, Surface catalycity, Recombination, Atmospheric entry, Arc-heated facility
Event Title:8th European Symposium on Aerothermodynamics for Space Vehicles
Event Location:Lissabon, Portugal
Event Type:international Conference
Event Dates:02. - 06. März 2015
Organizer:ESA
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 - Rückkehrtechnologie (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Über- und Hyperschalltechnologien
Deposited By: Esser, Dr.-Ing. Burkard
Deposited On:19 Aug 2015 16:32
Last Modified:19 Aug 2015 16:32

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