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Share  Title: Temperature measurements during Reentry

 

 
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This experiment is aimed at simulating the re-entry conditions encountered during the actual flight in a plasma arc jet facility and investigating the temperature distribution along with the thermal expansion on the surface of a re-entry vehicle in order to study the thermal breakdown mechanisms of the carbon-carbon composite of the leading edge of the vehicle.This test facility is designed to test a suitably sized block of the Thermal Protection System (TPS) made up of carbon carbon composite that is currently used in these vehicles and also any newly developed materials of appropriate size for evaluation as a possible replacement. The final outcome of this project is intended to be a quantitative relation that indicates the robustness of a material and thereby its ability to qualify as a material of choice for reusable re-entry vehicles.

 
 
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Keywords

Temperature  measurement  reentry  plasma  arc  jet  
composite  pyrometer  
 
 
 About This Document
 
 Subject Aeronautics and Astronautics
 Category White Paper
 Views 3913
 Downloads 274
 Added 12-08-09
 Contributor   sidpatel
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