Methodology and Results of Catalycity and Plasma Erosion Tests on FEI Components

941586

6/1/1994

Authors
Abstract
Content
A Flexible External Insulation (FEI) is being developed for the thermal protection of spaceplanes and re-entry capsules. Presently, forward extension of the FEI to locations of higher aerothermal loads is being studied. To evaluate the FEI under simulated re-entry conditions a test campaign has been planned and performed by the Rarefied Gas Dynamics Laboratory of the Russian Central Aerohydrodynamic Institute (TsAGI). Coated and non-coated FEI fabrics were exposed to a hypersonic high-enthalpy air flow in the VAT-104 plasma wind tunnel.
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DOI
https://doi.org/10.4271/941586
Pages
15
Citation
Shvedchenko, V., Zhestkov, B., Fischer, W., and Ebeling, W., "Methodology and Results of Catalycity and Plasma Erosion Tests on FEI Components," SAE Technical Paper 941586, 1994, https://doi.org/10.4271/941586.
Additional Details
Publisher
Published
6/1/1994
Product Code
941586
Content Type
Technical Paper
Language
English