AbstractEffects of variable thermal properties (specific heat and thermal conductivity) of the solid phase on the combustion of composite solid propellants are studied analytically. Both steady and unsteady burning are considered. It is shown that the effects of variable thermal properties are small and can be accounted for by choosing proper average values of specific heat and thermal conductivity.
Effect of variable thermal properties of the solid phase on composite solid propellant combustion
Acta Astronautica ; 58 , 12 ; 617-621
2006-01-09
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Effect of variable thermal properties of the solid phase on composite solid propellant combustion
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