Burn Rate Modelling of Solid Rocket Propellants (Short Communication)

Abstract

A generalised model of burning of a solid rocket propellant based on kinetics of propellant has been developed. A complete set of variables has been formed after examining the existing models. Buckingham theorem provides the functional form of the model, such that the existing models are the subcases of this generalised model. This proposed model has been validated by an experimental data.