Abstract
Thermal damage was applied to LX-17 at 190°C for several hours. The damaged LX-17 samples, after cooled down to room temperature, were characterized for their material properties, safety and performance. Mass losses upon thermal exposure were insignificant (<0.1 mass%). The damaged LX-17 samples expanded, resulting in a bulk density reduction of 4.3%. Subsequent detonation measurements (cylinder tests) were conducted on the thermally-damaged LX-17 samples. The results showed that the fractions of damaged LX-17 reacted were slightly lower than those of pristine LX-17. The thermally damaged LX-17 samples had average detonation velocity of 7.341 mm μs−1, lower than that (7.638 mm μs−1) of pristine LX-17. The average detonation energy density for the damaged LX-17 was 5.18 kJ cm−3, about 6.0% lower than the detonation energy density of 5.51 kJ cm−3 for the pristine LX-17. The break-out curves showed reaction zone lengths for pristine LX-17 and damaged LX-17 were similar but the damaged samples had ragged detonation fronts. DSC curves showed no significant difference between pristine LX-17 and damaged LX-17 with a peak temperature of 381°C observed.
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Hsu, P., Souers, C., De Haven, M. et al. Characterization of thermally-damaged LX-17. J Therm Anal Calorim 93, 311–317 (2008). https://doi.org/10.1007/s10973-007-8869-y
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DOI: https://doi.org/10.1007/s10973-007-8869-y