Solid rocket propellant transparency effect

on ignition by radiation

 

    Dragan Lemiæ

 

The influence of solid rocket propellant optical properties on the ignition process in the case of heat supply by radiation was analyzed. Temperature and concentration in the solid phase were calculated numerically. Transparency increase causes the extension of ignition delay time and the decrease of ignition temperature. The ignition process character is under the influence of the applied heat flux as well. The investigation results are presented in the form of tables and diagrams.

 

Ključne reči:   solid rocket propellants, combustion, ignition.

 

FUL TEXT