Shock tube measurement of explosive sensitivity
โ Scribed by M.H. Friedman
- Publisher
- Elsevier Science
- Year
- 1966
- Tongue
- English
- Weight
- 568 KB
- Volume
- 10
- Category
- Article
- ISSN
- 0010-2180
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โฆ Synopsis
A shock tube test is described, in which fine dusts or sprays o/explosive materials are ignited behindthe reflected shock, and the dependence o] the measured ignition delay on reflected shock temperature is determined. The test simulates the impact initiation of liquids and solids by bubble hot spots in a clean, controlled and weU-deflned ]ashion. From only a few tests, one can obtain (t) a valid measure o] the sensitivity o] the explosive, using only milligramme quantities o] material, and (2) inIormation about the physical and, in some cases, the chemical, mechanism o] the initiation o] the substance upon impact. The hot gaseous environment o] the sample is well defined through normal shock relations and the natu.re of the channel gas may be varied to study environmental effects. Test data on a number of explosives are presented and are interpreted in terms o] initiation mechanism. The experimental results suggest that hot spot temperatures required to initiate sensitive materials are between 500 ยฐ and 800ยฐC, and that bubble compression to ]orm hot spots is decidedly non-adiabatic.
๐ SIMILAR VOLUMES
Ignition times and OH concentration time histories for JP-10/O 2 /Ar mixtures have been measured behind reflected shock waves. Experiments were performed over the temperature range of 1200-1700 K, pressure range of 1-9 atm, fuel concentrations of 0.2% and 0.4%, and stoichiometries of U โซืกโฌ 0.5, 1.0,