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Estimating Thermal Decomposition Parameters for Lithium Hydride in a High Temperature Gas Flow

Authors: Tovstonog V.A. Published: 14.06.2018
Published in issue: #3(120)/2018  

DOI: 10.18698/0236-3941-2018-3-14-29

 
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes  
Keywords: lithium hydride, high temperature gas flow, heat-absorbing material, thermal decomposition, ablation, decomposition parameters

Operability of high-temperature power and propulsion systems largely depends on solving the problems of thermal protection of those structural elements that are subjected to high-enthalpy gas flows. For a wide range of varying thermal load parameters, ablative thermal protection offers the most opportunities. This protection is based on physical and chemical transformation laws and the products of destruction of thermal protection material actively responding to external heat loads. Selecting a thermal protection material requires data on properties as determined by planned operation conditions. We consider certain models and estimate thermochemical decomposition parameters for the case of lithium hydride in a high temperature flow of products of kerosene combustion in air. We show that this compound may serve as a highly efficient ablative thermal protection material over a certain range of thermal load parameters

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