Experimental and theoretical burning of solid rocket propellants near the pressure deflagration limit

Author:

Bruno Claudio,Riva Giulio,Zanotti Claudio,Dondè Roberto,Grimaldi Carlo,Luca Luigi De

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference22 articles.

1. Deflagration limits in the steady linear burning of a monopropellant with application to ammonium perchlorate;Johnson,1962

2. A model for ammonium perchlorate deflagration between 20 and 100 atm;Guirao;AIAA Journal,1971

3. An experimental study of the low pressure limit for steady deflagration of ammonium perchlorate;Cohen Nir;Combustion and Flame,1973

4. Low pressure burning of composite solid propellants;Steinz;Propellants, Manufacture, Hazards, and Testing,1969

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