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UPDATED ABLATION AND THERMAL RESPONSE PROGRAM FOR SPACECRAFT HEATSHIELD ANALYSIS Frank S. Milos, Yih-Kanq Chen, and Thomas H. Squire
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Document Date: 2006-07-27 09:08:15


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File Size: 4,04 MB

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Company

FIAT / Aerotherm Corporation / FIATv2 / NASA Ames Research Center / /

Country

United States / /

Currency

USD / /

Event

Business Partnership / /

Facility

College of Engineering / University of New Orleans / University of Maryland / /

IndustryTerm

gas density component / gas flow / internal energy balance / energy conservation / boundary layer gas / gas flux / transient thermal energy transport / representative applications / configuration management / incident energy / energy flux / chemical interactions / conduction heat flux radiative heat flux universal gas / mass transfer activation energy recovery / surface energy balance / chemical reaction / thermal analysis tool / computational tools / chemical constituents / gas blowing rate / ablation products / /

OperatingSystem

Linux / /

Organization

University of Maryland / U.S. Government / College of Engineering / University of New Orleans / National Aeronautics and Space Administration / ICCE / /

Person

Thomas H. Squire / Frank S. Milos / Galileo Probe Heatshield / H. Squire Thermal / Ai / /

Position

representative applications / RT / General / /

ProvinceOrState

Maryland / California / Colorado / /

Technology

radiation / sublimation / Linux / unix / ATM / heat transfer / simulation / /

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