A melhod for measuring the ignition energy of propellants using hot wirt~ at high hea't fluxes is described and the influence of pressure, propellant temperature and ignition rime is determined. Several experiments have shox~u good reproducibility of results using the equipment proposed. The differe
Ignition of a granular propellant bed
β Scribed by Anna E. Wildegger-Gaissmaier; Ian R. Johnston
- Publisher
- Elsevier Science
- Year
- 1996
- Tongue
- English
- Weight
- 894 KB
- Volume
- 106
- Category
- Article
- ISSN
- 0010-2180
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β¦ Synopsis
An experimental and theoretical study is reported on the ignition process of a low vulnerability ammunition (LOVA) propellant bed in a 127-mm (5-in) bore gun charge. The theoretical investigation was with a two-phase flow interior ballistics code and the model predictions showed the marked influence the igniter system can have on pressure wave development, flame spreading, and the overall interior ballistics performance. A number of different igniter systems were investigated in an empty and propellant-filled gun simulator. Pressure, flame spreading, and high-speed film records were used to analyze the ignition/combustion event. The model predictions for flame spreading were confirmed qualitatively by the experimental data. Full-scale instrumented gun firings were conducted with the optimized igniter design. Pressure waves were not detected in the charge during the firings. Model predictions on overall interior ballistics performance agreed well with the firing data.
π SIMILAR VOLUMES
By means of a dual-flash X-ray technique, propellant grain velocities during ignition have been determined for the Navy 5-in./38 gun. At the completion of ignition, the velocity profile along the grain bed is sharply peaked with maximun velocity at the propellant free surface.
Ignition delay of phenol-formaldehyde composite propellants was measured by a hot plate technique. The activation energy for the preignition reactions has been computed using the Arrhenius type expression for ignition delay.
The ignition of composite solid propellants by CO 2 laser irradiation at low pressures has been investigated experimentally. Three ignition modes are found at subalJnospheric pressures: self-sustaining ignition, non-self-sustaining ignition, and pulsating ignition. Here, the self-sustaining and the