Estimation of burning characteristics of AP/HTPB composite solid propellant using a sandwich model

Author:

Vijay ChaitanyaORCID,Ramakrishna P.A.

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Reference52 articles.

1. Understanding Aerospace Chemical Propulsion;Mukunda,2017

2. Burning mechanism of ammonium perchlorate propellants. Part II, theory of burning of composite solid propellant;Summerfield,1958

3. A model of composite propellant combustion including surface heterogeneity and heat generation;Hermance;AIAA J.,1966

4. A model of composite solid-propellant combustion based on multiple flames;Beckstead;AIAA J.,1970

5. Distribution functions for statistical analysis of monodisperse composite solid propellant combustion;Glick;AIAA J.,1976

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