caa a22 4500 475810570 CHVBK 20180406123757.0 cr unu---uuuuu 170329e20000701xx s 000 0 eng 10.1007/BF02699478 doi (NATIONALLICENCE)springer-10.1007/BF02699478 Glotov O. Institute of Chemical Kinetics and Combustion, Siberian Division, Russian Academy of Sciences, 630090, Novosibirsk aut Condensed combustion products of aluminized propellants. II. evolution of particles with distance from the burning surface [Elektronische Daten] [O. Glotov] Condensed combustion products of a model propellant on the basis of ammonium perchlorate and aluminum were studied using the sampling technique. The granulometric composition of combustion products and the content of metal aluminum in particles of size from 1.2 µm to maximum were determined within the pressure range of 0.6-7.5 MPa at a distance from the burning surface up to 190 mm. A multimode structure of mass distributions of oxide particles within the size range of 1.2-40 µm was found. An empirical dependence of burnout of metal aluminum from agglomerates on the residence time of particles in the plume of combustion products of the propellant sample was obtained. Kluwer Academic/Plenum Publishers, 2000 Combustion, Explosion and Shock Waves Springer US 36/4(2000-07-01), 476-487 0010-5082 36:4<476 2000 36 10573 https://doi.org/10.1007/BF02699478 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/BF02699478 text/html Onlinezugriff via DOI NATIONALLICENCE 100 1- Glotov O. Institute of Chemical Kinetics and Combustion, Siberian Division, Russian Academy of Sciences, 630090, Novosibirsk aut NATIONALLICENCE 773 0- Combustion, Explosion and Shock Waves Springer US 36/4(2000-07-01), 476-487 0010-5082 36:4<476 2000 36 10573 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer