1. V. A. Babuk, V. A. Vasilyev, and V. V. Sviridov, “Formation of condensed combustion products at the burning surface of solid rocket propellant,” in: V. Yang, T. B. Brill, and W. Z. Ren (eds.), Progress in Astronautics and Aeronautics, Vol. 185: Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics, Ch. 2.21, AIAA, Reston (2000), pp. 749–776.
2. V. A. Babuk, V. A. Vasilyev, A. A. Glebov, et al., “Combustion mechanisms of AN-based aluminized solid rocket propellants,” in: L. T. DeLuca, L. Galfetti, and R. A. Pesce-Rodriguez (eds.), Novel Energetic Materials and Applications, Proc. of the 9th Int. Workshop on Combustion and Propulsion, Paper No. 44, Grafiche GSS, Bergamo, Italy (2004), pp. 44-1–44-20.
3. O. G. Glotov and V. Ya. Zyryanov, “Condensed combustion products of aluminized propellants. I. A technique for investigating the evolution of disperse-phase particles,” Combust., Expl., Shock Waves, 31, No. 1, 72–78 (1995).
4. O. G. Glotov, “Condensed combustion products of aluminized propellants. II. Evolution of particles with distance from the burning surface,” Combust., Expl., Shock Waves, 36, No. 4, 476–487 (2000).
5. O. G. Glotov, “Condensed combustion products of aluminized propellants. III. Effect of an inert gaseous combustion environment,” Combust., Expl., Shock Waves, 38, No. 1, 92–100 (2002).