Detailed Characterization of Hypervelocity Firings in a Long 120-MM Gun
Carl R. Ruth, Albert W. Horst
Abstract
Carl R. Ruth, Albert W. Horst
Abstract
The applicability of lumped-parameter interior ballistic models to very high velocity guns is limited by the use of a superimposed pressure gradient to approximate the relationship between the space mean, breech, and projectile base pressures. Even modern two-phase flow interior ballistic models, specifically formulated to address the hydrodynamics of the problem, are largely untested in such regimes. Serious attempts to develop high-velocity solid propellant guns, however, require an accurate modeling capability for concept screening and charge optimization. Firings were conducted in a long 120-mm gun (Ballistic Tube) at a propellant charge to projectile mass (C/M) ratio of about 3 to provide muzzle velocities in the 2 - 2.5 km/s range. The tube was instrumented with pressure gages at 14 locations to determine the experimental pressure-displacement profile. Results were compared to predictions of a classical lumped-parameter code, a state-of-the-art two-phase flow model, and a lumped-parameter code with a recently developed pressure gradient.
OpenAlex reports 1 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
The applicability of lumped-parameter interior ballistic models to very high velocity guns is limited by the use of a superimposed pressure gradient to approximate the relationship between the space mean, breech, and projectile base pressures. Even modern two-phase flow interior ballistic models, specifically formulated to address the hydrodynamics of the problem, are largely untested in such regimes. Serious attempts to develop high-velocity solid propellant guns, however, require an accurate modeling capability for concept screening and charge optimization. Firings were conducted in a long 120-mm gun (Ballistic Tube) at a propellant charge to projectile mass (C/M) ratio of about 3 to provide muzzle velocities in the 2 - 2.5 km/s range. The tube was instrumented with pressure gages at 14 locations to determine the experimental pressure-displacement profile. Results were compared to predictions of a classical lumped-parameter code, a state-of-the-art two-phase flow model, and a lumped-parameter code with a recently developed pressure gradient.
Key concepts: Projectile, Propellant, Internal ballistics, Mechanics, Muzzle velocity, Hypervelocity, Muzzle, Physics