Preliminary research of composite rocket propellants with hexogen and titanium oxide powder

Author:

Rodić Vesna,Bogosavljević Marica,Milojković Aleksandar,Mijatov Slavko

Publisher

Centre for Evaluation in Education and Science (CEON/CEES)

Reference19 articles.

1. TERZIĆ,J. LEKIĆ,A. ZEČEVIĆ,B.: Prediction the Theoretical Interior Ballistic Properties of Solid Propellant Rocket Motors, 6th Seminar 'New Trends in Research of Energetic Materials' University of Pardubice, 23-25. April 2003, ISBN 0-7194-543-9, pp.420-435.;

2. VENKATACHALAM,S., SANTHOSH,G., NINAN,K.N.: High Energy Oxidisers for Advanced Solid Propellants and Explosives, Chapter 1 Introduction to Explosives and Propellants Advances in Solid Propellant Technology, P1 International HEMS1 Workshop, Ranchi, INDIA, 2002, pp.87-106.;

3. FIGUEIREDO,P.A., BROJO,F.M.: Theoretical analysis of ammoniumperchlorate based composite propellants containing small size particles of boron, 4th International Conference on Energy and Environment Research, ICEER 2017, 17-20. July 2017, Porto, PORTUGAL;

4. KUBOTA,N.: Combustion of Composite Propellants: Combustion of Composite Propellants, in Propellants and Explosives, Thermochemical Aspects of Combustion, Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim, GERMAMY. doi: 10.1002/9783527693481.ch7, 2015.;

5. BECKSTEAD,M.: Recent Progress in Modeling Solid Propellant Combustion, Combustion, Explosion and Shock Waves, November 2006, Vol.42, No.6, pp.623-641;

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