Condensed combustion products of aluminized propellants. II. evolution of particles with distance from the burning surface

О. Г. Глотов1
1Institute of Chemical Kinetics and Combustion, Siberian Division, Russian Academy of Sciences, Novosibirsk

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P. F. Belyaev, Yu. V. Frolov, et al.,Burning of Powdered Metals in Active Media [in Russian], Nauka, Moscow (1972).

E. W. Price, “Combustion of metallized propellants,” in: K. K. Kuo and M. Summerfield (eds.),Progress in Astronautics and Aeronautics, Vol. 90:Fundamentals of Solid Propellant Combustion. Chapter 14. Amer. Inst. of Aeronautics and Astronautics. New York (1984). pp. 479–514.

V. D. Gladun, Yu. V. Frolov, L. Ya. Kashporov, et al., “Agglomeration of powdered metal particles during combustion of composite condensed systems,” Preprint, Joint Inst. of Chem. Phys., Acad. of Sci. of the USSR. Chernogolovka (1977).

L. P. Bakhir, G. I. Levashenko, and V. V. Tamanovich, “Influence of the chemical composition of metallized propellants on the disperse composition, optical characteristics of oxide particles and flame emissivity,”Fiz. Goreniya Vzryva,16, No. 6, 10–16 (1980).

V. A. Babuk, V. P. Belov, V. V. Khodosov, and G. G. Shelyukhin, “Investigation of the agglomeration of aluminum particles in the combustion of metallized composite condensed systems,”Fiz. Goreniya Vzryva,21, No. 3, 20–25 (1985).

E. W. Price. R. K. Sigman, J. R. Sambamurthi, and C. J. Park, “Behavior of aluminum in solid propellant combustion,” AFOSR-TR-82-0964, Georgia Inst. of Technology (1982).

O. G. Glotov, V. E. Zarko, V. V. Karasev, and M. W. Beckstead, “Aluminum agglomeration in solid propellants: Formulation effects.” in:Propellants, Explosives. Rockets, and Guns: Proc. of the Second Int. High Energy Materials Conference and Exhibit (December 8–10, 1998), IIT Madras, Chennai, India (1998), pp. 131–137.

N. N. Ivanov and A. N. Ivanov, “Devices and setups of contact diagnostics and their use in studies of high-temperature two-phase flows,”Fiz. Goreniya Vzryva,27, No. 6, 87–101 (1991).

G. I. Levashenko and L. P. Bakhir, “Method for the withdrawal of particles formed in the combustion of metallized condensed systems in a constant-pressure chamber,”Fiz. Goreniya Vzryva,9, No. 2, 330–331 (1973).

B. N. Fedorov, Yu. L. Plechov, and É. M. Timokhin, “Particle size of aluminum oxide particles in the combustion products of condensed substances,”Fiz. Goreniya Vzryva,18, No. 1, 22–27 (1982).

V. A. Babuk, V. P. Belov, and G. G. Shelukhin, “Combustion of aluminum particles on composite condensed systems under low and high pressures,”Fiz. Goreniya Vzryva,17, No. 3, 26–31 (1981).

J. K. Sambamurthi, E. V. Price, and R. K. Sigmen, “Aluminum agglomeration in solid propellant combustion.”AIAA J.,22, No. 8, 1132–1138 (1985).

Tai-Kang Liu, Huey-Cherng Perng, Song-Ping Luh, and Fang Liu, “Aluminum agglomeration in AP/RDX/A1/HTPB propellant combustion.” AIAA Paper No. 91-1870 (1991), pp. 1–11;J. Propuls. Power,8, No. 6 (1992). pp. 1177–1184.

Tai-Kang Liu and Chi-Fa Hsich, “Analysis of agglomerate size from burning aluminized AP/RDX/HTPB propellants in quench bomb,”J. Propuls. Power,12, No. 5, 995–998 (1996).

J. Duterque, “Experimental studies of aluminum agglomeration in solid rocket motors,” in: 4th Intern. Symp. on Special Topics in Chemical Propulsion. ONERA TP 1996-48. Stockholm, Sweden (1996). (Available on the Internet: http://www.onera.fr/RECH/BASIS/public/web_fr/document/DDD/243366.pdf).

P. C. Braithwaite, W. N. Christensen, and V. Daugherty, “Quench bomb investigation of aluminum oxide formation from solid rocket propellants. Part I: Experimental methodology,” in: 25th JANNAF Combustion Meeting (Huntsville, AL), Chemical Propulsion Information Agency, Johns Hopkins Univ., Applied Physics Lab., CPIA-Pub-498-VI, Laurel, MD (1988). pp. 175–184.

17.M. Salita. “Quench bomb investigation of aluminum oxide formation from solid rocket propellants. Part II: Analysis of data,”ibid., in: pp. 185–197.

E. I. Gusachenko, V. P. Fursov, V. I. Shevtsov, et al., “Special features of agglomerate formation in combustion of composite propellants,” in:Physics of Aerodispersed Systems [in Russian], No. 21. Vishcha Shkola, Kiev Odessa (1981). pp. 62–66.

E. I. Gusachenko, L. N. Stesik, V. P. Fursov, and V. I. Shevtsov, “Investigation of the condensed combustion products of magnesium powders. I. Dependence on pressure.”Fiz. Goreniya Vzryva,10, No. 4, 548–554 (1974): “II. Dependence on particle size,”Fiz. Goreniya Vzryva,10, No. 5, 676–869 (1974).

J. L. Eisel, B. G. Brown, and E. W. Price, “Pressure, velocity, and geometry effect on Al2O3 produced during aluminized propellant combustion,”AIAA J.,13, No. 7, 913–917 (1975).

O. G. Glotov and V. Ya. Zyryanov, “Condensed combustion products of aluminized propellants. I. A technique for investigating the evolution of dispersed-phase particles,”Fiz. Goreniya Vzryva,31, No. 1, 74–80 (1995).

L. P. Bakhir and G. I. Levashenko, “Investigation of the drop size of the aluminum oxide near the burning surface of the propellant.”Fiz. Goreniya Vzryva,9, No. 6, 842–849 (1973).

V. M. Gremyachkin, A. G. Istratov, and O. I. Leipunskii, “Theory of burning of metal particles,” in:Physical Processes in Combustion and Explosion [in Russian], Atomizdat, Moscow (1980). pp. 4–68.

V. M. Gremyachkin, A. G. Istratov, V. I. Kolesnikov-Svinarev, et al., “Reaction zones in combustion of an aluminum drop in air under conditions of zero gravity and free fall,” in:Chemical Physics of the Combustion and Explosion Processes. Combustion of Condensed Systems [in Russian], Joint Inst. of Chem. Phys., Acad. of Sci. of the USSR, Chernogolovka (1977), pp. 78–81.

O. G. Glotov and V. Ya. Zyryanov, “The effect of pressure on characteristics of condensed combustion products of aluminized solid propellants.”Arch. Combust.,11, Nos. 3–4, 251–262 (1991).

V. A. Babuk, V. P. Belov, V. V. Khodosov, and G. G. Shelyukhin, “Study of the structure of agglomerates with combustion of aluminized mixed condensed systems,”Fiz. Goreniya Vzryva,24, No. 5, 52–57 (1988).

W. N. Brundige and L. H. Caveny, “Low burning rate aluminized propellants in acceleration fields,”AIAA J.,22, No. 5, 638–646 (1984).

W. R. Cofer, G. G. Lala, and J. P. Wightman, “Analysis of midtropospheric space shuttle exhausted aluminum oxide particles,”Atmospher, Environ.,21, No. 5, 1187–1196 (1985).

L. Caveny and A. Gany, “Breakup of Al/Al2O3 agglomerates in accelerating flowfields,”AIAA J.,17, No. 12, 1368–1371 (1979).

P. V. Novitskii and I. A. Zograf,Evaluation of the Measurement Result Error [in Russian], Énergoatomizdat, Leningrad (1985).

O. G. Glotov, V. E. Zarko, and V. V. Karasev, “Problems and prospects of investigating the formation and evolution of agglomerates by the sampling method,”Fiz. Goreniya Vzryva,36, No. 1, 161–172 (2000).

O. G. Glotov, V. E. Zarko, V. V. Karasev, and M. W. Beckstead, “Effect of binder on the formation and evolution of condensed combustion products of metallized solid propellants,” in:Combustion and Detonation: 28th Int. Annual Conf. of ICT. Report No. 75, Karlsruhe, Germany (1997). pp. 1–15.

R. W. Hermsen, “Aluminum oxide particle size for solid rocket motor performance prediction,”J. Spacecraft Rockets,18, No. 6, 483–490 (1981).