Projectile and method for sealing a projectile in a barrel
A barrel assembly for a weapon, said barrel assembly including a barrel; a plurality of projectile assemblies axially disposed in end to end abutting relationship within said barrel for operative sealing engagement with the bore of the barrel, each projectile including a projectile head and an integral cylindrical spacer portion extending axially and rearwardly from said projectile head; discrete propellant charges accommodated within said cylindrical spacer portion for propelling respective projectile assemblies sequentially through the muzzle of the barrel; ignition means for igniting said discrete propellant charges; and control means for selectively and sequentially actuating the ignition means. In one form, each projectile assembly further includes an internal wedging surface, at or adjacent the trailing end of said cylindrical extension which accommodates a tapered nose part of a following projectile, for expanding said trailing end into enhanced sealing engagement with the barrel upon engagement of said wedging surface with said tapered nose part.
1. A method of sealing a projectile in a barrel, including:
providing the projectile with a nose and a tail,
loading the projectile in the barrel whereby the tail of the projectile is adjacent the nose of a trailing projectile, each projectile being associated with a discrete propellant charge for sequentially and selectively propelling the respective projectiles from the barrel;
exerting a force to the projectile directed axially down the barrel so that the tail is forced onto the nose of the trailing projectile, and
in response to the force between nose and tail, expanding part of the projectile into a sealing contact with the bore of the barrel.
2. A method of loading according to claim 1 wherein the force is exerted on the projectile by a reaction to firing of a leading projectile.
3. A method of loading according to claim 1 wherein the force is exerted on the projectile before any projectiles are fired.
4. A method according to claim 1 wherein the projectile includes a spacer which limits displacement of the projectile down the barrel.
5. A method according to claim 1 wherein the tail includes a cylindrical portion which is expanded radially into contact with the bore.
6. A method according to claim 1 wherein the propellant is provided in a cylindrical extension of the tail.
7. A method according to claim 1 wherein the propellant charge for a projectile is provided in the barrel in a space behind the projectile's tail and about the nose of a trailing projectile.