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Mars entry simulation in the arc heated facility L2K

Gülhan, A. and Esser, B. and Koch, U. and Hannemann, K. (2002) Mars entry simulation in the arc heated facility L2K. 4th European Symposium Aerothermodynamics for Space Applications, Capua, 15.-18.10.2001.

Full text not available from this repository.

Abstract

Comparative tests using a cold wall heat flux sensor and the TPS basic material SiC were performed in the hypersonic high enthalpy flow of the arc heated facility L2K representing the Martian and air atmospheres. The emission spectroscopy technique was used for the measurement of the emission in the shock layer ahead the stagnation point model. Remarkable difference was noticed in the emission behaviour of these two atmospheres. The cold wall heat flux rate was measured with a Heat-Flux-Microsensor (HFM) based on thermopile technique. Completely different cold wall heat flux rates and surface temperature development on a SiC-probe were measured in air and Martian atmosphere at comparable gas mass flow rate and reservoir pressure levels. The nozzle flow and the flow field around the model was computed using CFD codes including chemical nonequilibrium processes.

Item URL in elib:https://elib.dlr.de/13868/
Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=2004,
Title:Mars entry simulation in the arc heated facility L2K
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Gülhan, A.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Esser, B.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Koch, U.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hannemann, K.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2002
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 665-672
Status:Published
Event Title:4th European Symposium Aerothermodynamics for Space Applications, Capua, 15.-18.10.2001
Organizer:ESA
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology
Deposited By: DLR-Beauftragter, elib
Deposited On:31 Jan 2006
Last Modified:14 Jan 2010 21:05

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