Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1717265 | Acta Astronautica | 2006 | 5 Pages |
Abstract
Effects 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.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Michael Shusser, Norman S. Cohen, F.E.C. Culick,