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7. Klager К., Zimmerman G.A., Steady Burning Rate and Affecting Factors: Experimental Results// AIAA Progress in Astronautics and Aeronautics.- 1992. -V.143. - Chapter 3. -P.59-109.

8. Beckstead M.W. A Model for Ammonium Nitrate Composite Propellant Combustion: In 26th JANNAF Combustion Meeting, Pasadena, CA, USA CPIA. - 1989. -V. 4. -№.529. - P. 213-230.

9. Kubota N. Survey of Rocket Propellants and Their Combustion Characteristics// AIAA Progress in Aeronautics and Astronautics.- 1984. -V. 90. - Chapter 1. - P. 21.

10. Korting P.A. et al.Combustion Characteristics of Low Flame Temperature, Chlorine-free Composite Solid Propellants// Journal of Propulsion and Power. -1990.-V. 6. - № 3.- P. 250-255.

11. Andreev K.K., Glaskova, A.P. A Comment to the Theory of Permissible Explosives// Proc. Acad. Sci. USSR (Doklady).- 1952.- V. 86. - P. 801-805.

12. Glaskova A.P. Effect des Catalyseurs Sur la Deflagration du Nitrate d¢Ammonium et de ses Melanges// Explosifs. - 1967.-№.1.- P. 5 -13.

13. Carvalheira P., Campos J., Gadiot G.M. et al. Burning Rate Modifiers for AN/HTPB-IPDI Composite Solid Propellants for Gas Generators: Proceedings of the 26th International Annual Conference ofICT, 1995.

14. Carvalheira P., Gadiot, G.M.H.J.L., and DeKlerk W.P.C. Mechanism of Catalytic Effects on PSAN/HTPB Composite Solid Propellants Burning Rates: Proceedings of the 25th International Annual Conference ofICT, 1994.

15. Menke К., Maub J.B., Brehler K.P. Characteristic Features of AN-GAP Propellants: AGARD Environmental Aspects of Rocket and Gun Propulsion, AalesundNorway, September 1994.

16. Zhao X.B., Hou L.F., Zang, X.P. Thermal Decomposition and Combustion of GAP/AN/Nitrate Ester Propellants: in «Solid propellant chemistry, combustion and motor interior ballistics»// AIAA Progress in Astronautics and Aeronautics. - 2000.-V. 185. - P. 413 -424.

17. Brewster M.Q., Sheridan T.A., Ishihara A. Ammonium Nitrate-Magnesium Propellant Combustion and Heat Transfer Mechanisms// Journal of Propulsion and Power. -1992.-V. 8.- №. 4.- P. 760 - 769.

18. Galeotta M. Metal Agglomeration and Combustion Mechanism of Ammonium Nitrate Based Rocket Propellants: Master¢s Thesis in Aerospace Engineering, SP Lab, Dipartimento di Energetica, Politecnico di Milano, Milan, Italy, 2003.