Impact-induced delayed detonation in an energetic material debris bubble formed at an air gap

Abstract

A planar model of a rocket motor has been developed that allows reaction in a central bore perforated by a projectile to be viewed with high-speed photography. Earlier work with this model showed that a “bubble” of propellant debris forms in the air gap between energetic material layers (bore region) as a result of projectile penetration of one of the layers. Ignition of the bubble occurs upon impact with the second layer, followed by a reaction ranging from mild burning to delayed delonation, depending on the width of the air gap, properties of the energetic material, and degree of confinement. The present paper presents the results of experimental and hydrocode studies to characterize the latter (delayed detonation) reaction. Results show that reaction initiates in the frontal portion of the bubble wall through mechanical (impact) shock. It then propagates backward through the bubble wall towards the first layer which then detonates. Detonation of the second layer occurs sympathetically. The reaction is bounded by a lower velocity limit and confined within a range of air gaps that increases with impact velocity. The upper-air-gap limit roughly coincides with the maximum expansion distance for the bubble before breakup, while the lower limit represents the minimum (threshold) damage level for detonation.