Esser, Burkard and Gülhan, Ali and Koch, Uwe and Keller, Karl (2009) Particle Erosion Tests on an Ablative Material in Martian Atmosphere. Proceedings of the 6th European Workshop Thermal Protection Systems and Hot Structures, 1. - 3. April 2009, Stuttgart, Germany.
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When planning and designing thermal protection systems for exploration missions to Mars, the specific properties of the Martian atmosphere must be accounted for. The atmosphere mainly consists of carbon dioxide (95.3%) with a minor fraction of nitrogen (2.7%) and smaller fractions of argon, oxygen and carbon monoxide. So, the chemical composition of the Martian atmosphere significantly differs from Earth atmosphere.
|Document Type:||Conference or Workshop Item (Speech)|
|Title:||Particle Erosion Tests on an Ablative Material in Martian Atmosphere|
|Keywords:||Ablative Material, Particle loaded flow, High enthalpy flow, Surface erosion, Arc Heated Facility|
|Event Title:||Proceedings of the 6th European Workshop Thermal Protection Systems and Hot Structures|
|Event Location:||Stuttgart, Germany|
|Event Type:||international Conference|
|Event Dates:||1. - 3. April 2009|
|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):||W - Grundlagen Raumtransport - Innovativer Thermalschutz (old)|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology|
|Deposited By:||Christine Adams|
|Deposited On:||25 Jan 2010 13:11|
|Last Modified:||07 Nov 2012 10:07|
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