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Title: Subatmospheric burning characteristics of AP/CTPB composite propellants with burning rate modifiers

Journal Article · · Combustion and Flame; (USA)
;  [1]
  1. Dept. of Aerospace Engineering, Indian Inst. of Tech., Madras-600 036 (IN)

While burning at subatmospheric pressure, composite propellant generally fume and under certain conditions eject partially reacted particles. This characteristic property is exploited in this study to understand the mechanism of burning rate modification. The additives CuCr{sub 2}O{sub 4}, Fe{sub 2}O{sub 3}, Sb{sub 2}O{sub 3}, Al(OH){sub 3} gel, and LiF were used with unmetallized AP/CTPB (carboxy terminated polybutadiene) composite propellants, and the following studies were done: burning rate measurements below and above atmospheric pressure (up to 70 bar); quantitative chemical analysis of fume deposits and ejected particles; and scanning electron microscope examination of the microstructure of the surface extinguished propellant samples. The results of the studies at subatmospheric pressure indicate that burning rate enhancers augment the AP/binder interfacial reactions, CuCr{sub 2}O{sub 4} decomposes into copper oxide and chromium oxide with net heat release, and if this occurs at the surface, it constitutes one route by which the burning rate could be enhanced, Fe{sub 2}O{sub 3} possibly enhances near-surface breakdown of heavy fuel molecules, and the melt layer on AP particles and the low-viscosity binder-melt, which exist when LiF is present in the propellants, possibly depress the burning rate.

OSTI ID:
6729092
Journal Information:
Combustion and Flame; (USA), Vol. 80:1; ISSN 0010-2180
Country of Publication:
United States
Language:
English

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