Thermoformed projectile cartridge
AssigneeThe United States of America as represented by the Secretary of the Navy
InventorJohn-Paul Shebalin
Life of this patent
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Abstract
An axisymmetric disk-shaped cartridge is provided for firing from a gun having a fluted bore. The cartridge is initiated by a firing pin and includes a primer core, a propellant charge, a booster charge, a projectile mass, an ablative cap and a ductile metal coating. The projectile mass is disposed over the booster charge while the ablative cap is disposed over the projectile mass. The coating and mass elongate and radially narrow to maintain axial symmetry while being accelerated along the bore.
Claims8
An axisymmetric disk-shaped thermoformed projectile cartridge (TPC) and a gun, said TPC comprising:
- a primer core that initiates in response to being struck;
- a propellant charge that annularly envelopes said core separated by an annular gap;
- a booster charge disposed over said propellant charge and within said annular gap, said booster charge initiating in response to said core, and said propellant charge initiating in response to said booster charge;
- a projectile mass disposed over said booster charge;
- an ablative cap disposed over said projectile mass;
- and
- a ductile metal coating that covers over said ablative cap, and around and under said propellant charge and said core, wherein said coating and said mass elongate and radially narrow to maintain axial symmetry while being accelerated along a fluted bore in the gun, said bore narrowing from a breech to a muzzle of the gun.
A gun having a fluted bore, said gun comprising:
- a firing pin within the bore that narrows from a breech to a muzzle;
- and
- an axisymmetric disk-shaped thermoforming projectile cartridge (TPC) for discharging from the bore, said TPC lengthening and narrowing while traversing through the bore, said TPC comprising:
- a primer core that initiates in response to being struck by said firing pin,
- a propellant charge that annularly envelopes said core separated by an annular gap,
- a booster charge disposed over said propellant charge and within said annular gap, said booster charge initiating in response to said core, and said propellant charge initiating in response to said booster charge,
- a projectile mass disposed over said booster charge,
- an ablative cap disposed over said projectile mass, and
- a ductile metal coating that covers over said ablative cap, and around and under said propellant charge and said core, wherein said coating and said mass elongate and radially narrow to maintain axial symmetry while being accelerated along the bore.
Dependencies are inferred from the claim text.